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NASA Technical Memorandum 100707 High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics and Space Administration Sclentiflc and Technical Information Office 1988 https://ntrs.nasa.gov/search.jsp?R=19890002769 2020-07-12T10:56:51+00:00Z

High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

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Page 1: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

NASA Technical Memorandum 100707

High Altitude

Atmospheric Modeling

Alan E. Hedin

Laboratory for Atmospheres

Goddard Space Flight Center

Greenbelt, Maryland

National Aeronautics andSpace Administration

Sclentiflc and TechnicalInformation Office

1988

https://ntrs.nasa.gov/search.jsp?R=19890002769 2020-07-12T10:56:51+00:00Z

Page 2: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics
Page 3: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Contents

I ,

2.

2.1

2.2

Introduction ................................................

Data sets studied ...........................................

General characteristics .................. ,...............

Coverage .................................................

.

3.1

3.2

3.3

Model comparisons ............................................

Model descriptions .......................................

Residual plots.. ................................ ,........

Results ..................................................

I

I

I

4

4

4

7

8

4. Summary of model strengths and weaknesses ................... 28

5. Conclusion .................................................. 29

References ...................................................... 31

Appendix A.

Appendix B.

Appendix C.

Appendix D.

Description of coverage files ...................... 35

Description of histogram files ..................... 37

Description of data comparison and coverage plots.. 41

Data set comparison summaries ...................... 77

PRECEDING PAGE BLANK NOT _I, MED

Ill

Page 4: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics
Page 5: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

I. Introduction

The purpose of this study is to compare existing total density data

with with several recent empirical models in order to assess current data

coverage, the accuracy of current empirical models, and where improvements may

be possible. The altitude range included in this study is 120 to 1200 km.

While techniques based on atmospheric drag effects provide total density

rather directly, the in situ mass spectrometer techniques provide densities of

individual constituents that must be su_ed to give total density, and this

was done for this study.

Several comparison studies have been made in the past (Marcos et al.,

1978; Hickman et al., 1979; Prag, 1983; Marcos, 1987) with somewhat differentdata sets and models, although there is some overlap in data and models with

the current study. A general result of previous studies was that density

models have an accuracy of around 15%, and this has not improved much over the

last 20 years. This study attempts to refine and quantify this assessment.

It produced extensive plots of data minus model residuals as a function of

various parameters to allow detailed comparisons and assessments.

This report describes the various products produced and gives some

general highlights of results. However, any study of this kind produces rich

detail and apparent anomalies that cannot be easily summarized, and interested

readers should consult the more detailed plots.

2. Data sets studied

2.1. General characteristics

The data sets utilized in the current report and areas of useful data

are summarized in Table I.

The Jacchia Drag data are total densities, deduced by the Smithsonian

Astrophysics Observatory (Jacchia and Slowey, 1965; 1970; 1972; 1975) from the

change of sateilite orbital elements as a result 6f air drag. The particular

data set used in this study was originally sent on tape by Jacchia to

F. Barlier in France, who kindly made a copy available to this author. These

data are believed to constitute the major proportion of the data used by

Jacchia in the generation of his models. The time (and thus spacial)

resolution of density derived from orbit change is generally rather coarse

with densities determined no more often than every three hours, and often one

day in contrast to tens of seconds or better for in situ data. Absolute

densities depend directly on the assumed drag coefficient. Jacchia (1977)

used 2.2 for atomic oxygen and a dependence on composition (altitude) as

specified by Cook (1976). Unfortunately, the Cook paper has a number of

possible algorithms and selectable parameters. The exact algorithm for drag

coefficients used by Jacchia is not specified in any known publication. This

situation could be important for determining drag and/or density at lower and

higher altitudes where atomic oxygen is not the major constituent, and theJacchia models (which were utilized to determine the composition dependent

drag coefficient) do not always give the correct composition. The data were

gatheredduring the decline of solar cycle 19 and the rise of solar cycle 20

over a wide range of latitudes.

Page 6: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table I. Summaryof data sets.

Name Method Dates Altitude FI0.7 Max Lat NumPts

Jacchia Drag 61001-70365 244-1200 70-176Barller Drag 64033-73058 123-735 68-176OGO-6 MS 69159-71177 394-1090 108-170AE-CMESA Accel 73353-76271 129-250 70- 93AE-COSS MS 74001-75161 130-837 70- 93AE-DMESA Accel 75280-76029 140-250 72- 79AE-DOSS MS 75291-76029 140-550 72- 78Cactus Accel 75178-79021 226-600 69-197AE-E MESA Accel 75335-78032 134-250 69-130AE-E OSS MS 75343-79049 134-544 69-197AE-E NACE MS 75335-81155 134- 69-225

DE-2 NACS MS 81220-83047 199-864 128-230

MSIS Comb MS 69178-83047 135-963 69-230

Drag - indicates density by orbit decay.

90 22124

90 11647

82 292470

68 1111O5

68 133405

9O 36743

90 49875

30 106933020 7O24O

20 181990

20 242931

90 292830

90 33181

Accel - indicates density by in situ accelerometer.

MS - indicates in situ mass spectrometer.

Page 7: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

The Barlier Drag data are total densities analogous to the Jacchia

densities but derived independently (Barlier et al., 1973) for generally

different satellites. These data are primarily useful for studying density

variations, as absolute values were normalized to Jacchia (1971) in an overall

sense. The data were taken during most of solar cycle 20 over a wide range oflatitudes.

The OGO-6 satellite (Carignan and Pinkus, 1968; Hedin et al., 1974)

was the first to obtain a long time series of fairly reliable mass spectro-

meter measurements. Perigee for most of the mission was near 400 km, and so

this satellite obtained more mass spectrometer data above 400 km than other

missions before or since. Total mass density was calculated as a summation of

measured atomic oxygen, helium, and molecular nitrogen. Measurements were

taken during the peak and decline of solar cycle 20 at all latitudes except

the extreme polar region.

The Atmospheric Explorer AE-C, -D, and -E satellites each carried an

in situ accelerome_er (MESA) (Champion and Marcos, 1973), open source mass

spectrometer (OSS) (Nier etal., 1973), a closed source mass spectrometer

(NACE) (Pelz et al., 1973) for composition measurements, and a closed source

mass spectrometer (NATE) (Spencer etal., 1973) for temperature and wind

measurements. The closed source geometry was thought to provide a better

determination of absolute density, while the more open source could better

detect reactive species. Absolute values from all three instruments are

comparable within the original target calibrations of about 15%. The NACEinstrument failed early in the AE-C flight. The entire AE-D satellite failed

after only about 3 months in operation. _All three instruments were highlysuccessful on AE_E with more data reduced for NACE. Total massdensity from

the mass spectrometers was calculated as a summation of measured atomic

oxygen, helium, argon, and molecular nitrogen. Total density from MESA was

based on a drag coefficient of 2.2 (Marcos etal., 1977). Measurements were

taken during solar cycle minimum at all latitudes and during the rise of cycle21 at low and midlatitudes.

The Castor satellite launched by CNES carried an accelerometer

(CACTUS) (Boudon and Barlier, 1979; Villain, 1980; Berger and Barlier, 1981)

for in situ density measurements. Measurements were taken during the rise of

solar cycle 21 at.low latitudes.

The Dynamics Explorer 2 satellite carried a mass spectrometer (NACS)

(Carignan etal., 1981) for in situ density and composition measurements, a

second mass spectrometer (WATS) (Spencer et al., 1981) for in situ temperature

and zonal wind measurements, and a Fabry-Perot spectrometer (FPI) (Hays et

al., 1981) for F-region temperature and meridional wind measurements. The

absolute density calibration of the mass spectrometers was not adequate due to

a failure of laboratory equipment and cannot be given much reliance. Total

mass density was calculated as a summation of measured atomic oxygen, helium,

argon, and molecular nitrogen. Measurements were taken during the peak and

decline of solar cycle 21 at all latitudes. They provide theonly set of high

solar activity high latitude mass spectrometer measurements available.

The MSIS combined density data set consists of separate data sets for

each atmospheric constituent that were formed from subsets selected from mass

spectrometer measurements on the OGO-6, AE-C, -D, -E, and DE-2 satellites

Page 8: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

described above, as well as the ESRO-4 (Trinks and yon Zahn, 1975), San Marco-

3 (Newton et al., 1974), and AEROS-A (Spencer et al., 1974) satellites and

numerous rockets. Data subsets were selected to provide the widest possible

coverage in geographical and geophysical parameters. These combined data sets

were used in the generation of the MSIS-86 model. While there is no parallel

set of total densities because the data were not originally selected with this

goal in mind (and thus without simultaneity in time for the various

constituents), the distribution and coverage of oxygen density are assumed to

represent the overall coverage in total density that could be obtained using

the mass spectrometer data. There is a similar combined data set for

temperature combining subsets from the AE-C, -D, -E, and DE-2 satellites,

rockets, and Millstone Hill, St. Santin, Arecibo, Jicamarca, and Malvernincoherent scatter stations.

2.2. Coverage,

More details on data coverage in terms of latitude, local time, day of

year, longitude, and UT can b% found in the coverage plots and data comparison

plots described in Appendix C, which are provided on microfich for each dataset.

The coverage of the MSIS combined data set for atomic oxygen, which is

essentially the coverage for goodpredictlon of total density from the MSIS-86

model, has been examined in more detail by sorting the data into bins based on

latitude, local time, day of year, universal time (UT), daily magnetic index

(Ap), mean FI0.7, daily minus mean FI0.7, and altitude. The results of this

binning procedure are computer readable files described in Appendix A. In

general, coverage is relatively poor at high magnetic activities, at altitudesbelow 200 km and above 800 km, and at high latitudes for low solar activity.

3. Model comparisons

3.1. Model descriptions

A large number of empirical models have been developed over the years.

The genealogy of these models is illustrated in Figure I. Hickman et al.

(1979) have given a brief but thorough description of the most common models

available at that time. Five specific models are selected for comparison with

data in the current study.

MSIS-86

The MSIS-86 model (Hedin, 1987) is the latest in the series of

empirical models of neutral temperature and density in the thermosphere (above

85 km) and lower exosphere based on in situ mass spectrometer and incoherent

scatter data. The model is dependent on user-provided values of day, time

(UT), altitude, latitude, longitude, local solar time, magnetic index (Ap), a

three solar rotation average I0.7-cm radio flux (FIO.7), and previous day

FI0.7. A history of three hour magnetic indices (ap) can be used for somewhat

better detail during magnetic storms. The model calculates neutral tempera-

ture, total density, and densities of N2, O , O, N, He, Ar, and H. The modelis based on a fit of in situ composition an_ temperature data from eight

scientific satellites (OGO-6, San Marco-3, Aeros-A, AE-C, -D, -E, ESRO-4, and

DE-2) and numerous rocket probes, as well as five ground-based incoherent

Page 9: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Year

1960

1965

1970

1975

1980

1985

ICAOARDC

HistoricaJ Development of Empirical Thermosphere Models

Primarily Total Density D=t= Primarily Temp. & Comp. Datafrom Satellite Drag from Ground and In-situ Instr.

I

DENSEL _ J60

LOCKHEED- (Jacchia}JACCHIA

USSA62

USSASuppl.

USSA76

J65

JACCHIA _L/"

WALKER-BRUCE

J70

GRAM(Justus)

ClRA61I

i HARRIS-J PRIESTER

'/I

II

CIRA65

J77

GRAM3

II

ii

I

Iil

t

I

'0, 72

ClRA86 (

OG06(Hedin)

M 1,M2 MSIS77 ESR04

(Thuillier) / (Hedin) (yon Zahn)DTM - r -'7 /

(Barlier) / l

AEROS MSIS(Kohnlein) UT/Long_

C(Kohnlein)

MSIS83

JMSIS86

Fig. i. History of empirical models.5

Page 10: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

scatter stations (Millstone Hill, St. Santin, Arecibo, Jicamarca, and

Malvern). The model supersedes the MSIS-83 model by inclusion of high

latitude, high solar activity data from the Dynamics Explorer satellite, and

the addition of atomic nitrogen to the gas species included in the model. The

MSIS-86 model was selected by COSPAR for inclusion in the next CIRA which has

yet to be published.

MSIS-8_

The MSIS-83 model (Hedin, 1983) is an empirical model of neutral

temperature and density in the thermosphere (above 85 km) and lower exosphere

based on in situ mass spectrometer and incoherent scatter data. The model is

dependent on user-provided values of day, time (UT), altitude, latitude,

longitude, local solar time, magnetic index (Ap), a three solar rotation

average I0.7-0m radio flux (FI0.7), and previous day FI0.7. A history of

three hour magnetic indices (ap) can be used for somewhat better detail during

magnetic storms. The model calculates neutral temperature, total density, and

densities of N2, 02, O, He, At, and H. The model is based on a fit of in situcomposition and temperature data from seven scientific satellites (OGO-6, San

Marco-3, Aeros-A, AE-C, -D, -E, and ESRO-4) and numerous rocket probes, as

well as five ground-based incoherent scatter stations (Millstone Hill, St.

Santin, Arecibo, Jicamarca, and Malvern). The model supersedes the MSIS-77

model by inclusion of data from the AE-D, AE-E, and ESRO-4 satellites, as wellas additional data from incoherent scatter stations that cover a wide range of

solar activities and the inclusion of longitude/UT variations. The MSIS-83

model extends the previous description of neutral parameters below 120 km to

the base of the thermosphere in a continuous manner.

MSIS-77

The MSIS-77 model (Hedin et al., 1977a; 1977b) is an empirical model

of neutral temperature and density in the thermosphere (above 120 km) and

lower exosphere based on in situ mass spectrometer and incoherent scatter

data. The model is dependent on user-provided values of day_ altitude,

latitude, local solar time, magnetic index (Ap), a three solar rotation

average I0.7-cm radio flux (FI0.7), and previous day FI0.7. The model

calculates neutral temperature, total density, and densities of N2, 02, O, He,Ar, and H. Themodel is based on a fit of in situ composition and temperature

data from five scientific satellites (AE-B, OGO-6, San Marco-3, Aeros-A, and

AE-C), as well as four ground-based incoherent scatter stations (Millstone

Hill, St. Santin, Arecibo, and Jicamarca). The model supersedes the OGO-6

model, which was based on data from only one satellite. The OGO-6 model is

now totally obsolete.

The MSIS-77 model used in this Study specifically did not include the

longitude/UT variations (Hedin et al., 1979), which are sometimes associatedwith this model name.

J77

The J77 model (Jacchia, 1977) is the latest in a series of empirical

models of neutral temperature and density in the thermosphere (abov e 90 km)

and lower exosphere based on atmospheric drag effects on satellite orbits.

The model is dependent on user-provided values of altitude, latitude, sun6

Page 11: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

declination, hour angle of sun, fraction of tropical year, invariant or

geomagnetic latitude, magnetic index (kp), a six solar rotation average of

FI0.7, and previous day FI0.7. The model calculates neutral temperature,

total density, and densities of N , O , O, He, At, and H. The model is basedprimarily on total densities deri_ed _rom changes in satellite orbits

(approximately 16 satellites during the 1960's) with an attempt to represent

changes in composition observed by OGO-6 and ESRO-4. The model differs from

the J71 and J70 models by the inclusion of elaborate formulations to describe

composition changes with local time and magnetic activity.

The code used for this model was generated from the original publica-

tion without later unpublished modifications.

JT__fio

The JTO model (Jacchia, 1970) is an empirical model of neutral

temperature and density in the thermosphere (above 90 km) and lower exosphere

based on atmospheric drag effects on Satellite orbits. The _odel is dependent

on user-provided values of altitude, latitude, sun declination, hour angle of

sun, fraction of tropical year, magnetic index (kp), a three solar rotation

average of FI0.7, and previous day FI0.7. The model calculates neutral

temperature, total density, and densities of N2, O2, O, He, At, and H. Themodel is based on total densities derived from changes in satellite orbits

(approximately 16 satellites during the 1960's). The model essentially

differs from the later J71 (Jacchia, 1971) by a smaller value of the 0/02

ratio at 150 km. The J70 model superseded the earlier J65 model (Jacchi_,

1965) by extending the model calculations below 120 km.

This model is the thermosphere end of the Marshall Space Flight Center

GRAM model, and the code for this model w_s obtained from MSFC.

3.2. Residual plots

Each of the data sets described above was divided into subsets

according to altitude and then compared to the five models in order to

calculate data residuals by taking the logarithm (base e) of the ratio of the

measured total density to model total density. The mean residual, standard

deviation of the residuals (square root of the sum of squares of each residual

minus the mean residual), and RMS (square root of the sum of squares of the

residuals) were calculated, and the residuals used to generate histogram plots

of the residuals and a large number of plots of residuals versus various

coordinates. The detailed description of the plots is given in Appendix C,

and the plots themselves are largely in microfich format. The binned data

used for the histogram plots (Figures CI and C2 of Appendix C) are also in a

series of ASCII computer files as described in Appendix B.

The total number of data points in some data sets was very large

(Table I). For handling and plotting convenience, a subset of points was

usually selected at random to bring the total points under 20,000. Previous

experience and statistics suggest this should be adequate for the current

comparisons. In any large data set, there are almost always a number of

points that are erroneous because of occasional problems somewhere in the

electronic or data-handling systems. Thus data points whose residuals from

both MSIS-86 and J70 were more than 10 times the estimated experimental error

Page 12: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

were discarded. Normally, only a few percent, and in no case more than 10%,of the points were dropped in this test. For each data set the exact samesetof points was finally comparedwith each of the five models and thus shouldprovide a reasonable relative comparison of the models. Judgments as to therelative value of various data sets is more problematic without considerableindividual attention to the nature of the problem points.

The model densities were calculated using the same (three solar cycle)average FI0.7 and one-day lag for each model. Also, most of the comparisonswere done using the daily Ap/Kp rather than the three-hour index. Limitedtests indicated a possible improvement of a percent or two (for all modelsexcept MSIS-77, which was not designed to use the more detailed index) inoverall standard deviations using the appropriate three-hour index.

3.3. Results

A sucmmry of the mean residuals for each of the data subsets under

magnetically quiet (Ap<=10) conditions is given in Table 2 as the logarit_m

(base e), along with the rank (I best to 5 worst) of each model with respect'

to this data subset in parenthesis after the residual. At the bottom is an

accumulation of how many data sets were ranked I to 5 for each model. These

rankings are plotted in Figure 2 and show that, except for MSIS-77, there isan approximately equal chance that any one of the models would give the lowest

mean residual for any of the data subsets. Also in the table is the number of

points and, in parenthesis after the number of points, the fraction of the

original data set used in the calculation.

The average over all data subsets for the models is -.02, -.O1, -.12,

-.01, -.04 for MSIS-86, -83, -77, J77, and J70, respectively. In other words,

the average difference in absolute densities between the existing data sets

and models is generally only a few percent. Averages based on mass spectro-

meter data are about 4% (.04 in logarithms) less than averages based on drag

data only. This is well within any a priori estimates of calibration errors.

Examination of specific data sets like Jacchia drag (used for generating theJacchia'models but not the MSIS models) or AE-E NACE (used for generating MSIS

models but not Jacchia models) confirms that there is little difference in

absolute values overall across models. The exception is MSIS-77, which was

generated with a database which did not have complete solar activity coverage,

but not surprisingly does well with, for example, AE-C data that were used in

generating this model

A summary of the overall standard deviations of the residuals for eachof the data subsets under magnetically quiet (Ap<=10) conditions is given in

Table 3 in the same format as Table 2, and the rankings are plotted in

Figure 3. Here we see a systematic trend toward lower standard deviations in

the later MSIS models. Taking a given data subset at random, one is more

likely to obtain the smallest standard deviations in the residuals using MSIS-

86. There are, of course, specific exceptions to this generalization such as

the'high altitude Jacchia drag data, where MSIS-86 and JTO are equivalent at

400-800 km and J70 is best above 800 km, and the counter example of OGO-6,

where MSIS-86 is best in the 400-800 km range. Small differences in ranking,

such as between J77 and J70, may not be significant, and it should be

remembered that in many cases the difference between best and worst is only a

few percentage points. Also, the data subsets are not entirely independent

8

Page 13: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 2. Overall mean (magnetically quiet).

Jacchiadrag

Barlierdrag

OGO-6ms

AE-C MESA

accel

AE-C OSS

ms

AE-D MESA

accel

AE-D OSS

ms

AE-D NACE

ms

Cactus

accel

AE-E MESAaccel

AE-E OSS

ms

AE-E NACE

ms

DE-2 NACS

ms

Alt Pts MSIS-86 MSIS-83 MSIS-77 J77 J70

200-400 3197 -.05 (3) -.05 (3) -.21 (4) -.03 (1) -.04 (2)4O0-800 6516 -.05 (1) -.06 (2) -.23 (3) -.05 (1) -.O6 (2)800-1200 3386 .O4 (2) .O4 (2) -.04 (2) -.O3 (1) -.05 (3)

120-200 1050 .02 (1) -.03 (2) -.02 (1) -.04 (3) -.07 (4)200-400 4761 .04 (3) .02 (I) -.06 (4) -.04 (3) .03 (2)

400-800 1447 .10 (2) .I0 (2) -.04 (I) .I0 (2) .15 (3)

200-400 1978(.20) .20 (2)

400-800 12863(.07) .20 (2)

120-200 5746(.25) .11 (3)

200-250 6101(.55) .02 (I)

.20 (2) .04 (1) .09 (2) .15 (3)

.20 (2) .04 (1) .21 (3) .25 (4)

.11 (3) .05 (2) .05 (2) .00 (1)

.04 (3) -.08 (4) .03 (2) -.03 (2)

120-200 6447(.65)-.01 (I) -.01 (I) -.05 (3) -.02 (2) -.07 (4)

200-390 6279(.2) .02 (2) .06 (3) -.08 (4) .09 (5) .01 (I)

120-200 11024(.7) -.03 (3)

200-250 4399 -.08 (3)

120-200 11787 -.01 (I)

200-390 I0923(.75)-.06 (3)

.00 (I) .00 (I) .02 (2) -.02 (2)

-.04 (2) -.11 (4) .01 (I) -.04 (2)

120-200 4614

200-400 5591

.01 (1) .01 (1) .04 (2) .01 (1)-.02 (1) -.20 (4) .03 (2) -.03 (2)

-.12 (3) -.09 (I) -.I0 (2) -.15 (4) -.18 (5)

-.21 (3) -.14 (I) -.33 (5) -.17 (2) -.22 (4)

200-400 11276(.I0)-.05 (2)

400-600 9808(.I0)-.02 (2)

120-200 11455(.45) .02 (2)

200-250 8363 -.01 (2)

120-200 11812(.62)-.01 (2)

200-400 9741(.12)-.03 (2)

120-200 7533 -.05 (1)200-400 10158(.14)-.09 (3)400-600 I0243(.20)-.17 (4)

200-400 6079(.08)-.23 (3)

400-800 3149(.20)-.17 (4)

-.05 (2) -.26 (4) -.03 (I) -.O8 (3)

-.O1 (I) -.36 (4) .01 (I) -.O7 (3)

.02 (2) -.01 (1) -.01 (1) -.03 (3)

.00 (1) -.06 (4) .05 (3) -.01 (2)

.00 (I) -.07 (4) -.05 (3) -.07 (4)

-.03 (2) -.15 (3) -.01 (I) -.03 (2)

-.05 (I) -.05 (I) -.05 (I) -.07 (2)

-.09 (3) -.22 (4) -.02 (2) -.07 (I)

-.14 (3) -.32 (5) -.12 (2) -.08 (1)

-.23 (3) -.33 (4) -.15 (1) - 22 (2)-.15 (3) -.38 (5) -.09 (1) -.14 (2)

Rank summary: I-6 1-11 I-8 1-11 I-5

2-11 2-10 2-3 2-11 2-12

3-10 3-8 3-3 3-5 3-74-2 4-0 4-12 4-I 4-5

5-3 5-I

Page 14: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

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w

C_S-,

Q)"00

s-

r..

10

Page 15: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 3. Overall Standard Deviation (magnetically quiet).

Jacchia

drag

Barlier

drag

OGO-6

ms

AE-C MESA

accel

AE-C OSS

ms

AE-D MESA

accel

AE-D OSS

ms

AE-D NACE

ms

Cactus

accel

AE-E MESA

accel

AE-E OSS

ms

AE-E NACE

ms

DE-2 NACS

ms

Aft Pts MSIS-86 MS15-83 MSIS-77 J77

------m_m----

200-400 3197 .15 (I) 16 (2) .18 (3) .15 (I)

400-800 6516 .26 (2) .26 (2) .29 (3) .25 (I)

800-1200 3386 .27 (3) .26 (2) .30 (4) .29 (3)

J70

.16 (2)

.26 (2)

.22 (I)

120-200 1050 .22 (1) .23 (2) .22 (1) .22 (1) .23 (2)200-400 4761 .20 (1) .20 (1) 21 (2) .21 (2) .21 (2)4OO-8OO 1447 .31 (1) .31 (1) .33 (3) .32 (2) .31 (1)

200-400 1978(.20) .14 (I)

400-800 12863(.07) .17 (I)

.14 (I) .14 (I) .16 (2) .17 (3)

.18 (2) .18 (2) .20 (3) .21 (4)

120-200 5746(.25) .16 (2) .16 (2) .15 (1) .18 (3) .18 (3)200-250 6101(.55) .21 (1) .21 (1) .21 (1) .21 (1) .21 (1)

120-200 6435(.65) .12 (2) .12 (2) .10 (1) .13 (3)200-390 6279(.2) .14 (1) .14 (1) .14 (1) .15 (2)

.13 (3)

.16 (3)

120-200 11024(.7) .i5 (2) .15 (2) .14 (1) .15 (2) .14 (1)200-250 4399 .18 (1) .19 (2) .18 (1) .18 (1) .18 (1)

.11 (1) .11 (1) .13 (2)

.18 (2) .18 (2) .17 (1)120-200 11787 .11 (1)200-390 10923(.75) .17 (1)

.11 (1)

.17(1)

120-200 4614 .17 (2) .17 (2) .16 (1) .16 (1) .16 (1)200-400 5591 .21 (2) .22 (3) .23 (4) .20 (1) .21 (2)

.15 (2) .18 (4) .16 (3) .16 (3)

.25 (2) .28 (5) .26 (3) .27 (4)

.12 (li .12 (1) .14 (2) .14 (2)

.18 (1) .19 (2) .20 (3) .20 (3)

.14 (2) .13 (1) .16 (4) .17 (5)

.18 (1) .21 (4) .20 (3) 21 (4)

.11 (1) .15 (2) .17 (4) .16 (3)

.19 (1) ..20 (3) .20 (2) .20 (2)

.19 (2) .22 (4) .18 (1) .20 (3)

200-400 11276(.I0) .14 (I)

400-600 9808(.IO) .24 (I)

120-200 11455(.45) .12 (1)200-250 8363 .18 (1)

12'0-200 11812(.62) .15 (3)

200-400 9741(.12) .19 (2)

120-200 7533 .11 (1)200-400 10158(.14) .20 (2)400-600 10243(.20) .19 (2)

200-400 6079(.08) .14 (1) .16 (2) .23 (5) .20 (4) .19 (3)400-800 3149(.20) .17 (1) .21 (3) .22 (4) .21 (3) .19 (2)

1-18 1-11 1-12 1-9 1-82-9" 2-16 2-5 2-8 2-83-2 3-2 3-4 3-9 3-94-0 4-0 4-6 4-3 4-3

5-2 5-I

]]

Page 16: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

u

cor_

4)

O"

>,

>,...,

m m

m (/1

_0 t"

(J 4D

4.m

m

co

(0 O

X [--

O O O O QO _ G) 'q" C_1m

s_,_S e_e G _o a_e_uaoJa d

0

_J

O"

,.-I

o

4-)

b0

E

0

"0

"o

"o

_J

ob_

°,_

w

c.

'00

12

Page 17: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

because of the grouping of instruments on the same satellite. Yet, for

reasons not understood, the various instruments on a given satellite do not

always give the same density, and it is not usually clear which one is right.

A summary of the mean residuals for each of the data subsets under

magnetically active (Ap>10) conditions is given in Table 4 in the same format

as Table 2, and rankings are plotted in Figure 4. The features are much the

same as for quiet conditions. The average over all data subsets for the

models iS -.03, -.01, -.07, .01, -.08 for MSIS-86, -83, -77, J77, and J70,

respectively. The MSIS-77 and J70 models have the most change in mean value

(about 4%) with increasing magnetic activity.

A stm_nary of the overall standard deviations of the residuals for each

of the data subsets under magnetically active (Ap>10) conditions is given inTable 5 in the same format as Table 2, and the rankings are plotted in

Figure 5. The features are much the same as for magnetically quiet conditions

except J77 has systematically higher standard deviations.

The models were also ranked for several specific types of variations

in Tables 6-10 and Figures 6-10 using data for all magnetic activities. Herethe standard deviation of the means of the binned data were calculated and

used for ranking. Table 6, for example, was taken from the plots showing

average residuals in l-hour bins as a function of local time (e.g., Figure C4

of Appendix C). If the data and model variations as a function of latitude

were the same, and the coverage for other important parameters, such as local

time, is either the same for each bin or correctly modeled, then the plotted

averages should be equal, and the standard deviation of these average values

zero. Coverage in other parameters is rarely perfect, but this plot and

ranking still emphasize selected types of variations. The local time ranking

(Table 7) corresponds to Figure C5, the mean FI0.7 ranking (Table 8) to Figure

C6, the daily FI0.7 ranking (Table 9) to Figure C7, and the magnetic activity

(Ap) ranking (Table 10) to Figure C19. The models are about equal in

predicting overall latitude variations (Figure 6), except for J77, which issomewhat worse. For local time variations (Figure 7) and daily FI0.7

variations (Figure 9), the later models are systematically better. For mean

FI0.7 variations, the models are about equal, except MSIS-77 is worse. For

magnetic activity variations (Figure 10), the later models are only slightly

better, and J77, worse.

A summary of the data comparisons on a data-set by data-set basis is

given in Appendix D with the attempt to identify variations that could

fruitfully be examined further. The most frequently noted residual trends (in

order) involved altitude, daily FIO.7 (daily minus mean), magnetic activity,

and annual (or semiannual) variations. The altitude trends could be a

combination of measurement problems and model problems. All of these trends

deserve careful Study by looking for similarities and differences between thedifferent data sets. Since these trends are handled by the model(s) in an

overall sense, the presence of a trend in a particular data set presumably

indicates that the magnitude of that variation (like the semiannual variation)

depends on some other unidentified factor. Both this data set summary and the

preceding discussion of overall means and standard deviations provide only ahint of the rich detail, exceptions, and anomalies that can be found in the

comparison plots.

]3

Page 18: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 4. Overall mean (magnetically active).

Alt Pts MSIS-86 MSIS-83 MSIS-77 J77 J70

Jacchia

drag

200-400 3197

400-800 6516

800-1200 3386

-.05 (3) -.04 (2) -.16 (5)-.04 (I) -.04 (I) -.16 (3).04 (2) .06 (3) .02 (I)

.02 (I) -.12 (4)

.06 (2) -.16 (3)

.07 (4) -.12 (5)

Barlier 120-200 681

drag 200-400 2761400-800 824

.o0 (I) -.06 (3) -.03 (2) -.14 (5) -.09 (4)-.02 (2) -.04 (3) -.09 (5) .o0 (I) -.06 (4):04 (2) .05 (3) -.05 (3) .11 (4) .O0 (I)

OGO-6

ms

200-400 757(.20) .00 (I) -.03 (2) - 17 (4) - 05 (3) -.03 (2)

400-800 6557(.07) .15 (4) .14 (3) .02 (I) .23 (5) .12 (2)

AE-C MESA 120-200 5746(.25) .14 (5)

accel 200-250 6101(.55) .02 (I)

.13 (4) .10 (2)

.05 (3) -.03 (2)

.11 (3) .07 (I)

.07 (4) -.05 (3)

AE-C OSS 120-200 6447(.65) .01 (2) .01 (2) .00 (I)

ms 200-390 6279(.2) .06 (3) .10 (4) .02 (2)

.01 (2) -.02 (3)

.16 (5) .O0 (I)

AE-D MESA 120-200 11024(.7) -.03 (3) .00 (I) .04 (4)

accel 200-250 4399 -.08 (4) -.03 (I) -.05 (2)

.03 (3) -.02 (2)

.06 (3) -.06 (3)

AE-D OSS

ms

120-200 11787 -.01 (2)

200-390 10923(.75)-.06 (2)

.02 (3) .06 (4)

.O0 (I) -.12 (5)

.06 (4) .00 (I)

.09 (4) -.08 (3)

AE-D NACE 120-200 4614

ms 200-400 5591

-.09 (4) -.05 (2) -.02 (I) -.06 (3) -.13 (5)-.19 (3) -.11 (2) -.22 (4) -.07 (I) -.23 (5)

Cactus

accel

200'400 8701(.I0)-.02 (I) -.O2 (I) -.15 (4) -.03 (2) -.14 (3)

400-600 8348(.10) .OO (I) .03 (2) .23 (5) .15 (3) -.21 (4)

AE-E MESA 120-200 11455(.45) .06 (3)

accel 200-250 8363 .03 (2)

.07 (4) -.03 (2) -.06 (3) -.02 (I)

.O5 (4) .01 (I) .04 (3) -.03 (2)

AE-E OSS

mS'

120-20011812(.62) .02 (2) .02 (1) -.03 (4) -.11 (3) -.06 (4)200-400 9741(.12)-.03 (1) -.03 (1) -.12 (3) -.03 (1) -.09 (2)

AE-E NACE 120-200 7533 -.04 (I) -.04 (I) -.08 (2) -.15 (4) -.09 (3)

ms 200-400 10158(.14)-.O9 (3) -.07 (I) -.18 (5) -.08 (2) -.11 (4)

400-600 10243(.20)-.18 (3) -.15 (2) -.29 (4) -.14 (I) -.14 (I)

DE-2 NACS 200-400 12286(.08)-.28 (3) -.28 (3) -.35 (4) -.15 (I) -.26 (2)

ms 400-800 90,77(.20)-.17 (3) -.16 (2) -.31 (5) -.02 (I) -.22 (4)

Rank summary:

]4

I-8 I-9 I-5 I-7 I-62-8 2-8 2-7 2-4 2-6

3-9 3-8 3-3 3-9 3-7

4-3 4-4 4-8 4-6 4-7

5-I 5-6 5-3 5-3

Page 19: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

B

C

am_

C

rv

U w_

.¢.m

1.0

!

I

t_

o

m

O)

QO

m

m m

OJ

Q O Q (_

sl._$ el,e a jo a_e_uaoJa d

Q

0

!

OlI-..4

CO

CO(DOI

(.0m.-m¢

Ol

O0I

6Y)

(Y)

.,-q

p'q

.,-.4

(or-

c_

(D

r_0c_

boc-

=:

.,.-(

15

Page 20: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 5. Overall Standard Deviation (magnetically active).

Jacchia

drag

Barlier

drag

@30-6

ms

AE-C MESA

accel

AE-C OSS

ms

AE-D MESA

accel

AE-D OSS

ms

AE-D NACE

ms

Cactus

accel

AE-E MESA

accel

AE-E OSS

ms

AE-E NACE

ms

DE-2 NACS

ms

Aft Pts MSIS-86 MSIS-83 MSIS-77 J77

200-400 2464 .18 (1) .19 (2) .20 (3) .21 (4)400-800 4007 .29 (2) .30 (3) .31 (4) .29 (2)800-1200 2549 .29 (2) .30 (3) .33 (5) .32 (4)

120-200 1050 .22 (2) .22 (2) .22 (2) .23 (3)

200-400 2767 .20 (I) .21 (2) .22 (3) .23 (4)

400-800 824 .30 (2) .29 (I) .32 (4) .31 (3)

200-400 757(.20) .19 (I)

400-800 6557(.07) .20 (I)

120-200 12359(.25) .16 (2)200-250 11585(.55) .21 (2)

120-200 12370(.65) .13 (2)200-390 6279(.2) .15 (1)

J70

.18 (I)

.28 (I)

.23 (1)

.21 (I)

.21 (2)

.30 (2)

.19 (1) .20 (2) .21 (3) .21 (3)

.21 (2) .20 (1) .22 (3) .21 (2)

.16 (2) .15 (1) .21 (4) .18 (3).21 (2) .20 (1) .23 (3) .21 (2)

.13 (2) .11 (1) .16 (4) .14 (3)

.16 (2) .17 (3) .19 (4) .16 (2)

120-200 8907(.7) .15 (1) .15 (1) .15 (1) .17 (2) .15 (1)200-250 3723 .19 (1) .19 (1) .19 (1) .20 (2) .19 (1)

120-200 7608 .13 (1) .13 (1) .13 (1) .15 (3)200-390 7476(.75) .22 (2) .21 (1) .21 (1) .23 (3)

.14 (2)

.21 (1)

120-200 4016 .13 (1) .13 (1) .13 (1) .14 (2) .14 (2)200-400 5566 .22 (2) .22 (I) .23 (2) .24 (3) .22 (I)

200-400 8701(.10) .17 (1) .17 (1) .19 (2) .21 (3) .19 (2)400-600 8348(.10) .28 (1) .29 (2) .30 (3) .31 (4) .30 (3)

.13 (1) .13 (1) .16 (3) .15 (2)

.18 (2) .18 (2) .20 (4) .19 (3)

120-200 8289(.45) .t3 (1)200-250 5582 .17 (1)

120-200 7868(.62) .16 (2)200-400 7854(.12) .19 (1)

.15 (1) .15 (1) .19 (4) .18 (3)

.20 (2), .22 (4) .23 (5) .21 (3)

120-200 6766 .13 (1) .13 (1) .17 (3) .19 (4)200-400 9079(.14) .23 (2) .22 (1) .24 (3) .23 (2)400-600 7987(.20) .23 (1) .23 (I) .27 (2) .23 (1)

.16 (2)

.23 (2).23 (1)

200-400 12286(.08i 16 (I)

400-800 9077(.20) ,24 (I).17 (2) .21 i5) .20 (4) .18 (3)

.27 (3) .28 (4) .26 (2) .24 (1)

Rank summary: 1-18 1-14 1-11 1-1 1-102-11 2-12 2-6 2-6 2-113-0 3-3 3-6 3-10 3-84-0 4-0 4-4 4-11 4-0

5-2 5-I

]6

Page 21: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

J_

¢0

>_t

> ••.., -_,4=t ,O_

u G3

m m

U

.- r-_

1--.

i

I.O

0

0qm

' I

CO

,.q-

O)

)

m

I

I

,0)

CO

I i

0 0(I0 CD

1 , !o o'q" C_i

aae_uao_a d

Q

I

co

co.s"

coCOI

O3

CO

COO0I

co

o3

0

>

p'4

,--4

cJ

boa_E

0

,,..4

r_

j..)co

0

E_

17

Page 22: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 6. Latitude Standard Deviation.

Jacchia

drag

Barlier

drag

@30-6ms

AE-C MESA

accel

AE-C OSS

ms

AE-D MESA

accel

AE-D OSS

ms

AE-D NACE

ms

DE-2 NACS

ms

Alt Pts MSIS-86

200-400 5661 .03 (I)

400-800 10529 .05 (2)

800-1200 5935 .O8 (3)

120-200 1731 .07 (2)

200-400 7528 .03 (I)

400-800 2271 .08 (3)

200-400 2735(.20) .04 (I)

400-800 19420(.O7) .03 (2)

120-200 18105(.25) .04 (1)200-250 17686(.55) .03 (1)

120-200 19050(.65) .05 (2)200-390 18897(.2) .04 (3)

MSIS-83 MSIS-77 J77 J70

.04 (2) .O5 (3) .04 (2) .03 (I)

.O7 (3) .08 (4) .04 (I) .04 (I)

.06 (2) .08 (3) .08 (3) .05 (1)

.07 (2) .06 (1) .10 (3) .07 (2).03 (1) .03 (1) .03 (1) .04 (2).o8 (I) .o7 (2) .08 (3) .o8 (3)

Rank summary:

.O6 (2) .07 (3) .O8 (4) .06 (2)

.03 (2) .02 (I) .O5 (3) .O6 (4)

.o4 (I) .04 (I)

.o5 (3) .04 (2)

.12 (3)

.o7 (4).09 (2).04 (2)

.04 (I) .04 (I) .O8 (3) .08 (3)

.01 (2) .03 (2) .04 (3) .03 (2)

120-200 19931(.7) .04 (2) .05 (3) .04 (2) .O8 (4)

200-250 8122 .O5 (I) .07 (3) .05 (I) .06 (2)

120-200 19365 .04 (2)200-390 18399(.75) .06 (3)

.03 (1)

.05 (1)

.04 (2) .02 (1) .07 (3) .04 (2)

.05 (2) .04 (1) .06 (3) .o6 (3)

120-200 8630 .10 (4) .09 (3) .06 (1) .07 (2) .11 (5)200-400 11157 .06 (1) .09 (4) .06 (1) .08 (3) .07 (2)

200-400 18365(.08) .03 (1)400-800 12226(.20) .03 (1)

I-92-6

3-4

4-I

.05 (2) .05 (2) .06 (3) .05 (2).04 (2) .04 (2) .08 (3) .03 (1)

1-42-10

3-54-I

1-10 1-2 1-62-6 2-3 2-9

3-3 3-12 3-34-I 4-3 4-I

5-O 5-O 5-I

]8

Page 23: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

4"*

C4;r_

m

oF-

50"q"

m

CGram

C

n-

com

4,a

m

&.

>

"o

a.%

.J

00 •m

_D

(5

m

0(D

s_$

J , J

O_

CXl

OJ

0 0 0

0D,."9

D-.D,-"9

D,.

t".!

OO

O9

COO0!

O_

OO

m

CJ)

OO!

OO_M..'4

"w

0

r-

Q

.,-4

m>

QJ-o

4.3

J.J

m,..M

o

b_

J._r-m

"0

o

,d

19

Page 24: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 7. Local Time Standard Deviation.

Jacchia

drag

Barlier

drag

OGO-6

ms

AE-C MESA

accel

AE-C OSS

ms

AE-D MESA

aecel

AE-D OSS

ms

AE-D NACE

ms

Cactus

accel

AE-E MESA

accel

AE-E OSS

ms

AE-E NACE

ms

DE-2 NACS

ms

Alt Ptso

200-400 5661

400-800 10529

800-1200 5935

b_m_

MSIS-86 MSIS-83 MSIS-77 J77 J70

.03 (1) .04 (2) .03 (1) .05 (3) .o_ (2)

.06 (2) .07 (3) .07 (3) .07 (3) .03 (I)

.07 (2) .07 (2) .14 (4) .12 (3) .05 (1)

120-200 1731

200-400 7528

400-800 2271

.06 (I) .07 (2) .06 (I) .08 (3) .o9 (4)

.02 (I) .03 (I) .02 (2) .04 (2) .03 (2)

.04 (I) .04 (I) .06 (3) .06 (2) .04 (I)

200-400 2735(.20) .13 (2)

400-800 19420(.07) .04 (I)

120-200 i8105(.25) .03 (2)

200-250 17686(.55) .04 (2)

120-200 19050(.65) .04 (1)200-390 18897(.2) .02 (1)

.12 (1) .12 (1) .12 (1) .12 (1).04 (1) .04 (1) .06 (2) .06 (2)

.03 (2) .02 (I) .07 (3) .07 (3)

.04 (2) .03 (I) .07 (3) .07 (3)

.04 (1) .04 (1) .05 (2) .06 (3).03 (2) .02 (1) .05 (3) .05 (3)

120-200 19931(.7) 10 (1) .11 (2) .12 (3) .15 (4) .10 (1)200-250 8122 .09 (2) .I0 (3) .I0 (3) .09 (2) .08 (I)

120-200 19365 .10 (2)200-390 18399(.75) .11 (2)

.09 (1) .09 (1) .09 (1) .10 (2)

.11 (2) .10 (1) .13 (4) .12 (3)

120-200 8630 .10 (4) .09 (3) .06 (1) .08 (2) .10 (4)200-400 11157 .12 (1) .13 (2) .13 (2) .12 (1) .13 (2)

200-400 19977(.10) .02 (1)400-600 18156(.10) .03 (1)

120-200 19744(.45) .03 (1)200-250 13945 .05 (1)

120-200 19680(.62) .02 (1)200-400 17595(.12) .02 (1)

120-200 14290 .03 (1)200-400 19237(.14) .03 (1)400-600 18230(.20) .04 (2)

200-400 18365(.08) .06 (1)400-800 12226(.20) .08 (1)

.03 (2) .05 (3) .09 (5) .o7 (4)

.04 (2) .o9 (4) .o8 (3) .o8 (3)

.04 (2) .04 (2) .04 (2) .08 (3)

.06 (2) .06 (2) .10 (3) .10 (3)

.03 (2) .04 (3) .10 (5) .09 (4)

.03 (2) .04 (3) .09 (4) .09 (4)

.03 (I) .06 (2) .I0 (4) .09 (3)

.04 (2) .06 (4) .07 (5) .05 (3)

.03 (I) .I0 (4) .04 (2) .05 (3)

.06 (1) .10 (3) .07 (2) .07 (2)

.09 (2) .10 (3) .09 (2) .09 (2)

Rank summary: 1-19

2-9

3-04-I

I-9

2-173-34-0

1-112-53-94-45-0

1-32-10

3-94-4

5-3

I-6

2-7

3-11

4-5

5-0

2O

Page 25: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

es,m.

tn

¢o

ot--

_=J_

¢0

03c-o

E.m>.

M

=ram

oJ

m

q.

Ioc3m

I i I

co

C_J

! I Io 0GD CD

s".=S e _.e13

!

! i I0 o_r ¢_1

_o a_e_uaaJa d

0t".-

.-a

o

r"..I

03

03_0

I

03

03:Z

¢DO0

!

O3

CO3E

0

o_,_L,

:>

.t,.4

,--I

0o

o

e..

21.

Page 26: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Jacchia

drag

Barlier

drag

OGO-6ms

AE-C MESA

accel

AE-C OSS

ms

Cactus

accel

AE-E MESA

accel

AE-E OSS

ms

AE-E NACE

ms

DE-2 NACS

mS

Table 8. Mean FI0.7 Standard Deviation.

Alt Pts

200-400 5661

400-800 10529

800-1200 5935

120-200 1731

200-400 7528

4O0-800 2271

200-400

,ill illiliJll II

MSIS-86 MSIS-83 MSIS-77 J77 J70

.05 (2) .04 (1) .05 (2) .06 (3) .05 (2)

.11 (2) .11 (2) .13 (3) .09 (1) .11 (2)

.08 (2) .08 (2) .11 (3) .13 (4) .07 (1)

.05 (3) .04 (2) .06 (4) .03 (1) .03 (1)

.03 (1) .04 (2) .04 (2) .04 (2) .03 (1)

.07 (2) .07 (2) .08 (3) .07 (2) .06 (I)

2735(.20) .04 (1) .06 (3) .05 (2) .05 (2)

400-800 19420(.07) .I0 (2)

120-200 18105(.25) .01 (2)

200-250 17686(.55) .04 (2)

120-200 19050(.65) .05 (3)200-390 18897(.2) .01 (1)

200-400 19977(.IO) .09 (4)

400-600 18156(.I0) .11 (3)

.05 (2).10 (2) .08 (1) .13 (3) .10 (2)

.01 (2) .00 (I) .02 (3) .04 (4)

.04 (2) .05 (3) .02 (I) .04 (2)

.05 (3) .03 (1) .04 (2) .06 (4)

.02 (2) .O5 (3) .02 (2) .02 (2)

.09 (4) .08 (3) .06 (2) .06 (1)

.10 (2) ,11 (3) .07 (1) .11 (3)

200-250 13945 .09 (1) .09 (2) .09 (2) .09 (3) .04 (3)

200-400 17595(.12) .06 (I)

200-400 19237(.14) .07 (2)400-600 18230(.20) .06 (2)

200-400 18365i.08) .07 (I)

400-800 12226(.20) .08 (I)

.06 (I) .06 (I) .06 (I) .06 (I)

.06 (I) .o9 (4) .o8 (3) .08 (3)

.05 (I) .08 (4) .O7 (3) .O8 (4)

.o8 (2) .15 (4) .09 (3) .08 (2)

.10 (2) .11 (3) .12 (4) ,10 (2)

Rank summary:I-7 I-4 I-4 I-5 I-6

2-9 2-13 2-4 2-6 2-8

3-3 3-2 3-8 3-7 3-34-I 4-I 4-4 4-2 4-3

22

Page 27: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

t.)r_

m

4-)

oi--

n_

om

L

t_

0m

[.I,

u

0

m

CO

0

I ' I

O_ Cq

, I , ! , !0 0 0CD _r C_

B_,BQ j0

0D,.

D-.D,-"9

D-.D,.

!

O3

CO"5"

C_

!

I--4

-s"

I

C_OD

I

O3

",s"

0

t-o

.,,-(

c_°,.-Ic_c_>

D,.-

c_r,.

f-c_Q)p_

o

_D

e-c_f,.,

Q;

o

r..

23

Page 28: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 9. Daily Minus Mean FI0.7 Standard Deviation.

Jacchia

drag

Alt Pts MSIS-86 MSIS-83 MSIS-77 J77

200-400 5661 .06 (2) .06 (2) .05 (I) .08 (4)

400-800 10529 .09 (3) .08 (2) .13 (5) .06 (1)800-1200 5935 .07 (1) .07 (1) .11 (4) ,09 (2)

Barlier 120-200 1731 .04 (I) .04 (2) .04 (I) .05 (3)

drag 200-400 7528 .01 (I) .O1 (I) .03 (2) .O8 (3)400-800 2271 ,08 (I) .07 (I) .06 (3) .15 (2)

OGO-6 200-400 2735(.20) ,07 (2) .07 (2) .06 (1) .13 (3)ms 400-800 19420(.07) .03 (I) .04 (2) .05 (3) .11 (4)

AE-C MESA 120-200 18105(.25) .06 (3)accel 200-250 17686(.55) .09 (3)

J70

.07 (3)

.10 (4)

.lO (3)

.05 (4)

.09 (4)

.18 (I)

•14 (4)

•12 (5)

.05 (2) .04 (I) .05 (2) .08 (4)

.08 (2) .05 (I) .05 (I) .I0 (4)

AE-C OSS 120-200 19050(.65) .06 (4) .05 (3) .03 (1) .04 (2)ms 200-390 18897(.2) .05 (2) .05 (2) .04 (I) .05 (2)

.06 (4)

.04 (I)

AE-D MESA 120-200 19931(.7) .10 (3) .11 (4) .10 (3) .06 (2) .05 (1)accel 200-250 8122 .12 (3) .14 (4) .08 (2) .06 (I) .06 (I)

AE-D OSS 120-200 19365 .01 (1) .02 (2) .02 (2) .01 (1)ms 200-390 18399(.75) .04 (2) .05 (3) .01 (I) .01 (I)

AE-D NACE 120-200 8630 .06 (4) .06 (3) .05 (I) .04 (2)

ms 200-400 11157 .09 (I) .I0 (2) .04 (2) .06 (I)

Cactus 200-400 19977(.10) ,11 (4) .08 (3) .08 (3) .06 (1)accel 400-600 18156(.I0) .I0 (2) .08 (I) .12 (4) .11 (3)

AEmE MESA 120-200 19744(.45) .02 (2)

accel 200-250 13945 .02 (I)

.02 (2)

,01 (1)

AE-E oss 120-200 19680(62) .03 (2)ms 200-400 17595(.12) .03 (1)

.04 (4)

.05 (2)

.07 (2)

.11 (3)

.01 (1) .02 (2) .04 (3) .05 (4)

.02 (1) .02 (1) .05 (3) .04 (2)

.02 (1) .03 (2) .05 (3) .06 (4)

.03 (1) .04 (2) .10 (4) .08 (3)

AE-E NACE 120-200 14290 .01 (1) .01 (1) ,03 (3) ,03 (3)ms 200-400 19237(.14) .08 (2) .08 (2) .09 (3) .09 (3)

400-600 18230(.20) .06 (I) .07 (2) .07 (2) .08 (3)

.07 (2) .08 (3) .08 (3)

.09 (3) .06 (I) .I0 (4)DE-2 NAGS 200-400 18365(.08) .06 (I)

ms 400-800 12226(.20) .08 (2)

.02 (2)

.07 (1)

.11 (4)

.i0 (4)

.11 (5)

Rank summary:1-12 I-9 1-11 I-7 I-6

2-9 2-13 2-8 2-7 2-5

3-5 3-5 3-7 3-11 3-4

4-3 4-2 4-2 4-4 4-125-I 5-0 5-2

24

Page 29: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

I

_/'GO

I=m

r_

m

I

I

= I0

--'_ "O'q" I

° I__ J

o

"- ]0 m

0o

I ' i

I I1 I0 0

III

1 , I'qr oJ

j0 a_e_ua0Ja d

O

D',..!

I

cr)..s-,

I

O')

r.l)

o

4O

>

r,..

E

I

"M(

r.o

o

fT.

25

Page 30: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Table 10. Ap Standard Deviation.

Jacchia

drag

nm_

Alt Pts

200-400 5661

400-800 10529

800-1200 5935

ii O iilli

MSIS-86 MSIS-83 MSIS-77 J77

.10 (1) .11 (2) ,14 (3) .16 (4).19 (3) .18 (2) .21 (5) .20 (4).21 (3) .19 (2) .22 (4) .24 (5)

Barlier 120-200 1731

drag 200-400 7528400-800 2271

J70

.lO (1)

.17 (I)

.16 (I)

OGO-6

ms

.09 (2) .08 (1) .08 (1) .12 (3) .08 (1).08 (1) .09 (2) .11 (3) .12 (4) .09 (2)

.11 (2) .09 (I) .11 (2) .12 (3) .13 (4)

200-400 2735(.20) .12 (2)

400-800 19420(.07) .12 (I)

AE-C MESA 120-200 18105(.25) .07 (2)accel 200-250 17686(.55) .10 (2)

120-200 19050(.65) .09 (3)200-390 18897(.2) .08 (2)

.12 (1) .14 (2) .15 (3) .14 (2)

.13 (2) .14 (3) .16 (4) .14 (3)

.07 (2) .06 (I) .17 (4) .11 (3)

.I0 (2) .O9 (I) .14 (4) .12 (3)

.08 (2) .06 (I) .15 (5) .I0 (4)

.07 (I) .I0 (3) .12 (4) .08 (2)AE-C OSS

ms

AE-D MESA 120-200 19931(.7) .O7 (I) .07 (I) IIO8 (2)

accel 200-250 8122 .09 (I) .09 (I) .09 (I)

AE-D OSS

ms

120-200 19365 .10 (I)

200-390 18399(.75) .16 (2)

Cactus

accel

200-400 19977(.10) .11 (3)400-600 18156(.10) .18 (2)

AE-E MESA 120-200 19744(.45) .07 (I)

accel 200-250 13945 .13 (2)

AE-E OSS

ms

120-200 19680(.62) .13 (3)200-400 17595(.12) .11 (2)

AE-E NACE

ms

120-200 14290 .08 (I)

200-400 19237(.14) .17 (3)

400-600 18230(.20) .11 (2)

.11 (3)

.lo (2)

.10 (t) .10 (1) .10 (1)

.15 (1) .15 (1) .19 (3)

.o8 (2)

.09 (1)

.11 (2),16 (2)

.09 (I) .I0 (2) .12 (4) .I0 (2)

.16 (I) .17 (2) .25 (4) .17 (2)

.07 (1) .07 (1) .17 (3) .12 (2)

.12 (1) .12 (1) .13 (2) .12 (1)

.12 (2) .11 (1)

.10 (1) .11 (2)

.08 (1) .09 (2).16 (2) .14 (1).12 (3) .14 (4)

DE-2NACS I200 -400 18365(.08) .09 (I)

ms 400-800 12226(.20) .15 (I)

.13 (3i

.16 (3)

.17 (4)

.16 (2)

.io (I)

.11 (3) .13 (4) .16 (5)

.20 (3) .23 (5) .21 (4)

.16 (4)

.11 (2)

.12 (3)

.20 (4)

.I0 (_)

.10 (2).18 (2)

Rank summary:1-10 1-14 1-11 I-2 I-7

2-11 2-10 2-7 2-3 2-12

3-6 3-3 3-4 3-8 3-44-0 4-0 4-3 4- 11 4-4

5-2 5-3 5-0

26

Page 31: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

m

ON

r,.,

>

>,

_,.-.

-" U

u tj

m

r0 _"'QD

O C0

F- _"

LD

oc_m

O"3

CO

{ , {O OG) (D

O4

s_s,e_eQ _0

I

0"3

{ , {O O'q" c_]

0

Op,....-)

{.,,.p,..

I

I

Z

I

0o,-¢

.,-¢

>

.,.-(

o,-¢

0.,-{

0.)

0

¢..

,.-"W

0z

2'7

Page 32: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

The ap history (in the case of MSIS-86 and "83) or lagged ap/kp (in

the case of J77 and J70) was tried for the Cactus data (low inclination orbit)

and DE-2 NACS data (polar orbit) in place of the more convenient daily Ap/Kp.

For Cactus the result for the magnetically active data (Ap>10) was a .02 (2%)

decrease in the overall standard deviation for MSIS-86 and -83, and a .01 (1%)

drop for J77. No change for the other models. For DE-2 there was a .O1

decrease for MSIS-86 and no change for the others. Plots against ap were a

bit smoother. It is apparent that on an overall statistical basis using the

three-hour ap's provides only a small improvement and no change in relative

rankings of the models. During a magnetic storm, of course, use of the three-

hour ap/kp can give dramatically better results, particularly for the timingof the onset. However, since high magnetic activity levels occur less

frequently than low magnetic activity levels, the use of the three-hour

indices has only a modest effect on overall statistics.

4. Summary of model strengths and weaknesses

MSIS-86

The MSIS-86 model is systematically better overall than any of the

other models in modeling of total density variations, and equivalent to theothers in absolute values. The standard deviation With respect to the Jacchia

drag data (200-400 km)is .15 (15%) under magnetically quiet conditions and.18 (18%) under active Conditions. The median standard deviation in

comparison to all the data sets under magnetically quiet conditions is about

.17 (17%), and the mean absolute error is -.02 (-2%). Some data sets, usually

with limited coverage, have lower standard deviations. The most obvious

deficiency is at high altitude, where _he database for generating this model

is weak, but where the accuracy of the data from both mass spectrometers and

drag techniques also needs careful assessment. The model is significantly

better than the Jacchia models in local time variations, particularly at lower

altitudes. Although not the focus of this study, a ranking of models for

predictions of temperature and composition variations based on the MSIS

combined data set would show a very strong preference for this model.

MSIS-83

The MSIS-83 model is overall slightly worse than MSIS-86. The

standard deviation with respect to the Jacchia drag data (200-400 km) is .16

(16%) under magnetically quiet conditions and .19 (19%) under activeconditions. The median standard deviation in comparison to various data sets

under magnetically quiet conditions is about .18 (18%) and the mean absolute

error is -.01 (-1%). However, this study did not emphasize, nor does an

overall assessment give a large weight to, the polar variations, which were

the focus of the changes between MSIS-83 and MSIS-86.

MSIS-77

The MSIS-77 model is slightly worse than MSIS-83 in overall standard

deviations, but distinctly worse in absolute densities. The standard

deviation with respect to the Jacchia drag data (200-400 km)is .18 (18%)

under magnetically quiet conditions and .20 (20%) under active conditions.The median standard deviation in comparison to various data sets under

magnetically quiet conditions is about .18 (18%) and the mean absolute error

28

Page 33: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

is -.12 (-12%). The greater errors here are largely a consequence of the morelimited data base, lacking coverage at high solar activities, as well ascoverage at high latitudes. The lack of longitude terms in the model shows upmost clearly in comparisons with DE-2 data. This model does as well or betterthan other models in comparisons with the OGO-6and AE-Cdata on which it washeavily based, but not as well as other models in comparisons with data setshaving wider coverage such as the Jacchia drag data. Although _itting the lowaltitude (below 200 km) Atmospheric Explorer variations satisfactorily, themodel formulation was not as general as used in the later models and cannot beextrapolated below the AE altitudes (about 140 km).

J77

The J77 model has the highest standard deviations under magneticallyactive conditions, but also with respect to latitude and local timevariations. The standard deviation with respect to the Jacchia drag data(200-400 km) is .15 (15%) under magnetically quiet conditions and .21 (21%)under active conditions. The median standard deviation in comparison tovarious data sets under magnetically quiet conditions is about .18 (18%), andthe mean absolute error is -.01 (-1%). The attempt to include bettercomposition and temperature variations through the cumbersome, time consuming,and nonphysical pseudo-temperature technique was only partly successful andappears to have detracted from the description of total densities.

J7__q0

The J70 model is slightly worse overall than MSIS-77 in total density

comparisons, but better than J77. The standard deviation with respect to the

Jacchia drag data (200-400 km) is .16 (16%) under magnetically quiet

conditions and .18 (18%) under active conditions. The median standard

deviation in comparison to various data sets under magnetically quiet

conditions is about .19 (19%), and the mean absolute error is -.04 (-4%).

This model is distinctly better than other models at higher altitudes (above

800 km) and usually worse at the lowest altitudes (less than 200 km). Between

200 and 800 km, J70 and MSIS-86 have equivalent standard deviations in

comparison to the drag related data sets, except Cactus, where J70 is slightly

worse. J70 is by far the worst model for temperature and composition

variations.

5. Conclusion

Five empirical models were compared with 13 data sets, including both

atmospheric drag based data and mass spectrometer data. The products of this

study included plots and ASCII files describing database coverage, extensive

comparison plots of data and models, and ASCII files of binned residuals.

Although the most recently published model, MSIS-86, was found to be

the best overall model, the general conclusion of previous studies wasreaffirmed: the best current accuracy is around 15%. A definite, but small

(few percent), improvement in total density accuracy of newer over older

models was discernible in this study.

It is clear that a model (like MSIS-77), which was generated from a

limited database, can be as good or better than other models for some data

29

Page 34: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

sets, but not as good for a wider range of data. Similarly, a later model

(like MSIS-86) may do worse than the earlier MSIS-77 on an earlier data set

(e.g., AE-C) because measurement errors or unidentified geophysical factorsmake the newer data sets not completely consistent with the older data sets.

This illustrates the obvious conclusion that a model based on or optimized for

a limited set of data can be very good for that data, but poor for other

data. Likewise, the addition of new data may make the model worse for older

data. However, unless we have reasons to discount certain measurements, the

broader based model is more likely to be best in comparison to a new

independent data set (or for a random prediction), and this is illustrated by

comparisons with the Cactus data, which were used for neither the MSIS orJacchia models.

The excellent overall agreement of the mass spectrometer based MSIS

models with the drag data, including both the older data from orbital decay

and the newer accelerometer data, suggests that the the absolute calibration

of the (ensemble of) mass spectrometers and the assumed drag coefficient in

the atomic oxygen regime are consistent to 5%. While the time may soon be at

hand to base a model on both the mass spectrometer and drag data, puzzling

disagreements in detail still remain at both high and low altitudes.

This study illustrates a number of the reasons for the current

accuracy limit. There appear to be sizable differences (order 20%) in overall

absolute values between some mass spectrometer missions (e.g., OGO-6 and DE-2)and most of the models and differences on the order of 10 to 15% between mass

spectrometers and drag measurements under certain conditions. This

illustrates the importance of reliable calibration techniques for mass

spectrometers and for the drag coefficient (especially when atomic oxygen is

not the major constituent) and the need for measurement accuracy at the level

desired for the model. There are trends still existing between certain data

sets and models with respect to FI0.7, Ap, and annual/semiannual variations.

These trends are apparently different from data set to data set and are

presumably the result of ancillary geophysical factors, which may or may not

be easily found and taken into account.

The largest variations in total density in the thermosphere are

already accounted for to a very high degree by existing models. In

statistical terms, more than 90% of the original variance in latitude, local

time, FI0.7, etc., are explained by existing models. The primary variations

were already well known at the time that J65 (Jacchia, 1965) was formulated

and this must explain in large part why progress has not been rapid in the

ensuing two decades (except in related areas like temperature, composition,and wind). Progress will likely 'continue to be modest in the future, although

there are areas with greater potential for improvement such as where we stillhave insufficient data (like the lower thermosphere or exosphere), where there

are disagreements in technique (such as the exosphere) that can be resolved,

or wherever generally more accurate measurements become available.

3O

Page 35: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

References

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atmosphere between 150 and 500 km, Space Res., 13, 349-355, 1973.

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Hedin, A. E., C. A. Reber, N. W. Spencer, H. C. Brinton, and D. C. Kayser,Global model of longitude/UT variations in thermospheric composition andtemperature based on _%ss spectrometer data, J. Geophys. Res, 84, I-9,

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empirical temperature profiles, Spec. Rep. 313, Smithsonian Astrophys.

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empirical temperature profiles, Spec. Rep. 3_2, Smithsonian Astrophys.

Observ., Cambridge, Mass., 1971.

Jacchia, L. G., Thermospheric temperature, density, and composition: new

models, Spec. Rep. 375, Smithson. Astrophys. Observ., Cambridge, MA, 1977.

Jacchia, L G., and'B. Slowey, Densities and temperatures from the atmospheric

drag on six artificial satellites, Spec. Rep., 171, Smithson. Astrophys.

Observ , Cambridge, Mass., 1965.

Jacchia, L G., and B. Slowey, A catalog of atmospheric densities from the

drag on five artificial satellites, S_pec. Rep., 326, Smithson. Astrophys.

Observ , Cambridge, Mass., 1970.

Jacchia, L G., and B. Slowey, A supplemental catalog of atmospheric densities

from satellite-drag analysis, Spec. Rep., 348, Smithson. Astrophys.

Observ , Cambridge, Mass., 1972.

Jacchia, L. G., and B. Slowey, A catalog of atmospheric densities from the

drag on five balloon satellites, Spec. Rep., 368, Smithson. Astrophys.

Observ., Cambridge, Mass., 1975.

Marcos, F. A., Accuracy of satellite drag models, AAS 87-552, AAS Publications

Office, San Diego, Calif., 1987.

Marcos, F. A., K. S. W. Champion, W. E. Potter, and D. C. Kayser, Density and

composition of the neutral atmosphere at 140 km from Atmosphere Explorer C

satellite data, Space Res., 17, 321-327, 1977.

Marcos, F. A., R. E. McInerney, and R. W. Fioretti, Variability of the lower

thermosphere determined from satellite accelerometer data, TR-78-O134, Air

Force Geophysics Laboratory, Hanscom AFB, Mass., 1978.

Newton, G. P., W. T. Kasprzak, and D. T. Pelz, Equatorial composition in the

137- to 225-km region from San Marco 3 mass spectrometer, J. Geophys.

Res., 79, 1929-1941, 1974.

32

Page 37: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Nier, A. 0., W. E. Potter, D. R. Hickman, and K. Maue_sberger, The open-sourceneutral mass spectrometer on Atmosphere Explorer-C, -D, -E, Radio Sci., 8,

271-276, 1973.

Pelz, D. T., C. A. Reber, A. E. Hedin, and G. R. Carignan, A neutral

atmosphere composition experiment for the Atmosphere Explorer-C, -D, -E,

Radio Sci., 8, 277-285, 1973.

Prag, A. B., A comparison of the MSIS and Jacchia-70 models with measured

atmospheric density data in the 120 to 200 km altitude range, Aerospace

Corporation report SD-TR-83-25, Los Angeles, Calif., 1983.

Spencer, N. W., H. B. Niemann, and G. R. Carignan, The neutral-atmosphere

temperature instrument, Radio Sci., 8, 284-296, 1973.

Spencer, N. W., D. T. Pelz, H. B. Niemann, G. R. Carignan, and J. R. Caldwell,

The neutral atmosphere temperature experiment, J. Geophys., 40, 613, 1974.

Spencer, N. W., L. E. Wharton, H. B. Niemann, A. E. Hedin, G. R. Carignan, and

J_ C. Maurer, The Dynamics Explorer wind and temperature spectrometer,

Space Sci. Instrum., 5, 417-428, 1981.

Trlnks, H., and U. yon Zahn, The Esro 4 gas analyzer, Rev. Sci. Instrum., 46,

213-217, 1975.

Villain, J. P., Traitement des donnees brutes de laccelerometre Cactus. Etude

des perturbations de moyenne echelle de la densite thermospherique, Ann.

Geophys., 36, 41-49, 1980.

33

Page 38: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics
Page 39: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Appendix A. Description of coverage files.

The following files contain the results of binning oxygen data used in

generating the MSIS-86 model. There are five files:

COVALLSA.DAT - binning for all mean FI0.7 values.

COVLOSA.DAT - binning for mean FI0.7 less than 100.

COVMLSA.DAT - binning for mean FI0.7 between 100 and 140.

COVMHSA.DAT - binning for mean FI0.7 between 140 and 180.

COVHISA.DAT - binning for mean FI0.7 greater than 180.

Each 80 byte record contains a 6 digit integer describing the bins based on

altitude, FI0.7 difference from the mean, day of year, local time, magnetic

activity (Ap), and universal time (UT), and 12 integers which indicate by a 0or I whether data was available in a 15 degree wide latitude bin between -90

and 90 degrees (e.g., the first of the twelve integers refers to -90 to -75

degrees and the last integer to 75 to 90 degrees). The fortran format

statement was (18,1216). The 6 digit bin code is AFDLPU where:

A : I indicates altitude less than 200 km_

2 indicates altitude between 200 and 400 km.

3 indicates altitude over 400 km.

F = I indicates daily minus mean FI0.7 less than -20.

2 indicates daily minus mean FI0.7 between -20 and 20.

3 indicates daily minus mean FI0.7 greater than 20.

D = I indicates days from I to 91.

2 indicates days from 91 to 182.

3 indicates days from 182 to 273.

4 indicates days greater than 273.L = I indicates local time between 0 and 4.

2 indicates local time between 4 and 8.

3 indicates local time between 8 and 12.

4 indicates local time between 12 and 16.

5 indicates local time between 16 and 20.6 indicates local time between 20 and 24.

P = I indicates daily Ap less than 10.

2 indicates daily Ap between 10 and 60.

3 indicates daily Ap between 60 and 110.

4 indicates daily Ap greater than 110.U = I indicates UT between 0 and 14400 seconds.

2 indicates UT between 14400 and 28800 seconds.

3 indicates UT between 28800 and 43200 seconds.2 indicates UT between 43200 and 57600 seconds.

2 indicates UT between 57600 and 72000 seconds.

2 indicates UT between 72000 and 86400 seconds.

There are 62208 possible bins and the overall coverage in each file was:

COVALLSA.DAT - 13187 or 21.2% for all solar activities.

COVLOSA.DAT - 4838 or 7.8% for low solar activity.

COVMLSA.DAT - 2235 or 3.6% for medium-low solar activity.

COVMHSA.DAT - 6384 or 10.3% for medium-high solar activity.

COVHISA.DAT - 3356 or 5.4% for high solar activity.

PRECEDING PAGE BLANK NOT FILMED

35

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_ ? _¢_ _ _ Ir_Z-

Page 41: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Appendix B. Description of histogram files.

Corresponding to each Figure CI and C2 (see Appendix C) an ASCII file

was produced containing informations on comparisons of a single data subset

with the five models. The file names start with HISTRHO followed by anabbreviation of the data set and the lowest altitude. Each file contains the

following information:

Data set name and model name;

Day interval;

Ranges for Ap, altitude, or other factors;

Number of points and overall standard deviation;

Root mean square error;

Title (unscaled histogram);

Two column list giving interval start and fraction of points in

interval. -99999 and 99999 used for data beyond -I to I;

Data set name and model name;etc.

The following is a partial listing of file HISTRHOAECMESA120:

AEC MESA

DAYS 73358

MAGNETIC INDEX (Ap)

ALTITUDE(km)NUMBER POINTS =

RMS ERROR = 0.1919779

UNSCALED HISTOGRAM

RHO - MSIS-86

74334

-99999.0000 0.0000-1.0000 0.0174

-0.9800 0.O000-0.9600 0.0174

-0.9400 0.0174_0.9200 0.0000

-0.9000 0.0174-0.8800 O.0174

-0.8600 0.0174

-0.8400 0.O000

-0.8200 0.0348

-0.8000 0.0174

-0.7800 0.0174

-0.7600 0.0348

-0.7400 0.0000

-0.7200 0.0000

-0.7000 0.0348

-0.6800 0.0000

-0.6600 0.0000

-0.6400 0.0000-0.6200 0.0174

-0.6000 0.0000

-0.5800 0.0000

-0.5600 0.0522

-0.5400 0.0174

5746

0.0000 10.0000 INCLUDED

120.0000 200.0000 INCLUDED

STD DEV = O. 592570 AVERAGE = 0.1072O4O

37

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38

-0.5200-0.5000-0.4800

-0.4600

-0.4400

-0.4200

-O.4OOO

-0.3800

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-0.3200

-O.3000-0.2800

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-0.2200

-0.2000

-0.1800

-0.1600

-0.1400

-0.1200

-0.1000

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-0.0200

0.0000

0.0200

0.0400O.060O0.08000.10000.12000.1400

0.1600

o.18oo0.2000

0_2200

0.2400

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0.3200

0.34000.3600O.38O0O.4000

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0.0870

0.0348

0.0174

0.0174

0.0000

0.0174

0.1392

0.0000

0.0348

0.1566

0.0522

0.1044

0.0696

0.1740

o.31330.2785

0.4525

0.5395

0.7832

0.9572

1.3401

2.0536

2.2973

3.1326

3.6199

4.1072

5.4647

5.6387

6.0564

5.89985.8127

5.9172

5.30805.3777

5.0818

3.9680

3.7591

3.3415

3.1500

2.7323

2.4365

1.8448

1.5837

1.0964

0.9050

0.6961

0.5221

0.4351

0_4699

0.2436

0.1392

0.1218

0.0696

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Page 43: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

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0

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39

Page 44: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics
Page 45: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Appendix C. Description of data comparison and coverage plots.

An example of the of the data coverage and model comparison plots

which were prepared for this project is shown in Figures CI to C34 for the

case of the Jacchia drag data 200 to 400 km subset compared to the MSIS-86

model. Some plots for other cases do not have all the information described

here because of changes made as the project progressed. These plots are from

a general plot program and some of the information is not of importance for

this project.

In the following descriptions the term data residuals indicates the

logarithm (base e) of the ratio of measured to model densities (or measured to

model difference in the case of temperature). The residuals are generally

averaged into appropriate bins and plotted as an average with an error bar.Error bars show the standard deviation of the data within each bin and the

plot number indicates the logarithm (base 2) of the number of points in eachbin.

On each plot the data set acronym, measured quantity (RHO means total

density), and model are given at the top center of the plot. At the top right

are the plot date and data file name. There are generally three lines of

compressed information at the bottom of each plot with the following meaning

(* indicates particular relevance for this project):

GRP - local data set identification number

* ALT LIM- altitude limits for this plot

ISK - number points skipped for extreme deviation

* SEL - if first integer is none zero data were limited

by the following two numbers. 7 indicates

a test on magnetic activity and thus Fig. AI

is for Ap from 0 to 10 and A2 covers Ap from11 to 400. 2 indicates a test on latitude.

* PTS PLT - indicates actual number of data points

involved in this plot.* AVG - overall average of logarithms of data to model

ratio for this plot.* SD - overall standard deviations of logarithms of

data to model ratio for this plot

A - binning intervals for abscissa and ordinate

if applicable.SW - MSIS switch settings

*DI,D2 - date limits for plotted data

ST,SX,SY - points skipped for SEL test, or beyondabscissa or ordinate limits.

SM - smoothing factor in contour plots (1.00 is none).

* DATA-MODEL - residual plot using given model

identification number or zero for no model.

* SD:DATA-MODEL - contour plot of standard deviationsof data residuals within each data bin.

* AVG,SD - for binned data, average and standarddeviation of binned data averages.

AVXL,AVXH - points beyond low and high abscissa on

histogram plots.

PR]_CEIr)[NG PAGE BLANK NOT FI_LMED

41

Page 46: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

* RMS- root mean square error for all points (fromAVG and SD values).

* DSD,MSD,R - for binned data, standard deviation of

bin averages of raw data, standard deviation

of bin averages of model values, and correlationcoefficient between data and model based on

bin averages.

42

Page 47: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

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Page 54: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

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Page 80: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics
Page 81: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Appendix D. Data set comparison summaries.

The following pages have a stum_ary of the data subset comparisons with

the models emphasizing observed trends for the different models.

PRI_CEDING PAGE BLANK NOT FILMED

"/7

Page 82: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-400FI0.7:70-190

Parameter: Total Density Dates: 61001-70365

Source: Jacchia sat. trk. Data File: DRAG

Best quiet mean: -.03 (J77) Worst quiet mean: -.21 (MSIS-77)

Best quiet SD: .15 (MSIS-86,J77) Worst quiet SD: .18 (MSIS-77)

Best active mean: .02 (J77) Worst active mean:-.16 (MSIS-77)

Best active SD: .18 (MSIS-86,J70) Worst active SD: .21 (J77)

Altitude: All equivalent.Residuals flat.

Latitude: MSIS-86

Residuals flat.

J70 least variance.

Local Time: MSIS-86 -77 least variance.

Residuals have terdiurnal variation for J77.

Mean FI0.7: MSIS-83 least variance.

Residuals flat.

Delta FI0.7: MSIS-77 least variance.

Residuals more positive with increasing activity for MSIS models and

more negative with increasing activity for J77 and J70.

Magnetic: MSIS-86 least variance.

Residuals near equator and poles flat except for MSIS-77 and J77.

Coverage to Ap 150 near equator and Ap 100 near pole.

Day/year: J70 least variance.

Residuals have annual, semiannual and longer trends.

Longitude/UT: Variances similar for all models.

Comments: Little overall difference between models except worse

for MSIS-77.

MSIS-86 trends: delta FI0.7 and annual.

78

Page 83: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 400-800FI0.7:70-190

Parameter: Total Density Dates: 61134-70364Source: Jacchia sat. trk. Data File: DRAG

Best quiet mean: -.05 (MSIS-86,J77) Worst quiet mean: -.23 (MSIS-77)

Best quiet SD: .25 (J77) Worst quiet SD: .29 (MSIS-77)

Best active mean:-.04 (MSIS-86,-83) Worst active mean:-.16 (MSIS-77,J77)

Best active SD: .28 (J70) Worst active SD: .31 (MSIS-77)

Altitude: J77 least variance.

Residuals flat but irregular for all models.

Latitude: J77 J70 least variance.

Residuals more negative at midlatitudes for MSIS-86 -83.

Local Time: J70 least variance.

Residuals have diurnal and semidiurnal for all models.

Mean FI0.7: J77 least variance.

Residuals irregularly more positive with increasing activity for MSIS

models.

Delta FI0.7: J77 least variance.

Residuals more positive with increasing activity for MSIS models and

more negative with increasing activity for J70.

Magnetic: MSIS-86 least variance.

Residuals flat but irregular. Coverage to Ap 150.

Day/year: J77 least variance.

Residuals have annual, semiannual and longer trends.

Longitude/UT: MSIS-86, J77, J70 least variance.Residuals may have second harmonic at lower latitudes for all models.

Comments: Little overall difference between models except worsefor MSIS-77.

MSIS-86 trends: latitude, local time, mean and delta FI0..7 and annual.

79

Page 84: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 800-1200FI0.7:70-190

Parameter: Total Density Dates: 61134-70364Source: Jacchia sat. trk. Data File: DRAG

Best quiet mean: -.03 (J77)

Best quiet SD: .22 (J70)Best active mean: .02 (MSIS-77)

Best active SD: .23 (J70)

Worst quiet mean: -.05 (J70)

Worst quiet SD: .30 (MSIS-77)Worst active mean:-.12 (J70)

Worst active SD: .33 (MSIS-77)

Altitude: MSIS-86 least variance.

Residuals irregular but flat for all models except more negative

at higher altitudes for J70.

Latitude: JTO has least variance.

Residuals more negative at midlatitudes for MSIS-86

Local Time: JTO least variance.

Residuals have diurnal and semidiurnal for all models.

-83.

Mean FI0.7: J70 least variance.

Residuals flat except more positive with increasing activity for MSIS-77.

Delta FI0.7: MSIS-86 , -831east variance.

Residuals more negative at low and high activity for MSIS models and

more negative with increasing activity for J77 and JTO.

Magnetic: J70 least variance.Residuals near equator and pole irregularly more negative with increasing

activity for all but J70. Coverage to Ap 150.

Day/year: J70 least variance.Residuals have annual, semiannual and longer trends.

Longitude/UT: J70 has least variance.

Comments: J70 best at this altitude.

MSIS-86 trends: latitude, local time, delta FI0.7 and annual.

8O

Page 85: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 120-200FI0.7:90-190

Parameter: Total Density Dates_ 66362-73057Source: Barlier sat. trk. Data File: DRAG

Best quiet mean: .02 (MSIS-86) Worst quiet mean: -.07 (J77)Best quiet SD: .22 (MSIS-86,J77) Worst quiet SD: .23 (MSIS-83,-77)Best active mean: .00 (MSIS-86) Worst active mean: .13 (J77)Best active SD: .21 (J70) Worst active SD: .23 (J77)

Altitude: J77 J70 least variance.Residuals more positive at lowest altitudes for MSIS models.

Latitude: MSIS-77 has least variance.

Residuals flat.

Local Time: MSIS-86 -77 least variance.

Residuals have diurnal and semidiurnal variation for MSIS-83, J77,and J70.

Mean FI0.7: J77 J70 least variance.

Residuals flat.

Delta FI0.7: Variances similar for all models.

Residuals flat for all models.

Magnetic: Variances similar for all models.

Residuals near equator more negative with increasing activity for all

models and no clear trend near poles. Coverage to Ap 200 near

equator and Ap 50 near poles.

Day/year: J70 least variance.

Residuals have annual, semiannual and longer trends.

Longitude/UT: Variances similar for all models.

Comments: Little overall difference between models but local time

and latitude variations somewhat worse for Jacchia models.

MSIS-86 trends: altitude, annual, and magnetic activity.

8]

Page 86: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-400FI0.7:70-190

Parameter: Total Density Dates: 64033-73058

Source: Barlier sat. trk. Data File: DRAG

Best quiet mean: .02 (MSIS-83) Worst quiet mean: -.06 (MSIS-77)

Best quiet SD: .20 (MSIS-86,-83) Worst quiet SD: .21 (MSIS-77,J70,J77)

Best active mean: .00 (J77) Worst active mean:-.09 (MSIS-77)

Best active SD: .20 (MSIS-86) Worst active SD: .23 (J77)

Altitude: MSIS-77 least variance.

Residuals more positive with increasing altitude except for MSIS-77.

Latitude: Variances similar for all models.

Residuals flat.

Local Time: MSIS-86 -77 least variance.

Residuals have terdlurnal variation for J77.

Mean FI0.7: MSIS-83

Residuals flat.

J77 leastvariance.

Delta FI0.7: MSIS-86 least variance.

Residuals more negative with increasing activity for J77 and J70.

Magnetic: MSIS-86 least variance.

Residuals near equator and poles more negative decreasing with

increasing activity for all models. Coverage to Ap 200 near

equator and Ap 150 near poles.

Day/year: MSIS-86 least variance.No obvious trends.

Longitude/UT: Variances similar for all models.

Comments: Little overall difference between models.

MSIS-86 trends: altitude and magnetic activity.

82

Page 87: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 400-800FI0.7:70-190

Parameter: Total Density Dates: 66011-73058Source: Barlier sat. trk. Data File: DRAG

Best quiet mean: -.04 (J77) Worst quiet mean:

Best quiet SD: .31 (MSIS-86,J70) Worst quiet SD:Best active mean: .00 (J70) Worst active mean:

Best active SD: .29 (MSIS-83) Worst active SD:

.15 (J70)

•33 (MSIS-77)

.11 (J77)

.32 (MSIS-77)

Altitude: J77 J70 least variance.

Residuals flat but irregular for ali models.

Latitude: Variances similar for all models.

Residuals flat for all models.

Local Time: MSIS-86, -83, J70 least variance.

Residuals have diurnal and semidiurnal for MSIS-77 and J77.

Mean FI0.7: Variances similar for all models except MSIS-77 worse.

Residuals flat for all models except MSIS-77.

Delta FI0.7: MSIS-77 least variance.

Residuals more negative with increasing activity for all models.

Magnetic: MSIS models least variance.

Residuals near equator and pole more negative with increasing activity

for all models. Coverage to Ap 150 near equator and Ap 100 near

pole.

Day/year: Variances similar for all models except MSIS-77 worse.

Residuals have annual, semiannual and longer trends.

Longitude/UT: Variances similar for all models.

Residuals may have second harmonic at lower latitudes for all modeIs.

Comments: Little overall difference between models.

MSIS-86 trends: delta FI0.7, annual, and magnetic activity.

83

Page 88: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-400FI0.7:100-170

Parameter: Total DensitySource: OGO-6 MS

Dates: 69187-71177Data File: OGORHOFIFTH

Best quiet mean: -.04 (MSIS-77) Worst quiet mean: .15 (J70)

Best quiet SD: .14 (MSIS) Worst quiet SD: .17 (J70)

Best active mean: .00 (MSIS-86) Worst active mean: .17 (MSIS-77)

Best active SD: .19 (MSIS-86,-83) Worst active SD: .21 (J77,J70)

Altitude: Insufficient coverage.

Latitude: MSIS-86 least variance.

Residuals more positive toward north pole for all models.

Local Time: Variances similar for all models.

Residuals flat but irregular.

Mean FI0.7: MSIS-86 least variance.

Residuals flat for all models.

Delta FI0.7: MSIS least variance.

Residuals more negative with increasing activity except flat for

MSIS-77.

Magnetic: MSIS-86 least variance.

Residuals more negative with increasing activity for all but MSIS-86.

Coverage to 160 Ap.

Day/year: Variances similar for all models.

Residuals more negative at beginning of 1971 for all models, but

less pronounced for Jacchia models.

Longitude/UT: Variances similar for all models.No obvious trends.

Comments: MSIS models best for standard deviations and overall.

MSIS-86 trends: delta FI0.7 and annual.

84

Page 89: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 400-800 Parameter: Total Density Dates: 69179-71177FI0.7:100-170 Source: OGO-6 MS Data File: OGORHOFIFTH

Best quiet mean: .04 (MSIS-77) Worst quiet mean: .25 (J70)

Best quiet SD: .17 (MSIS-86) Worst quiet SD: .21 (J77)

Best active mean: .02 (MSIS-77) Worst active mean: .23 (J77)

Best active SD: .20 (MSIS-86,-77) Worst active SD: .22 (J77)

Altitude: Variances similar for all models.

Residuals more positive at higher altitudes for all models.

Latitude: MSIS least variance.

Residuals more positive at midlatitudes for J77 and J70.

Local Time: MSIS least variance.

Residuals have semidiurnal or terdiurnal variation for J77 and J70.

Mean FI0.7: MSIS-77 least variance.

Residuals flat but irregular.

Delta FI0.7: MSIS-86 least variance.

Residuals more negative at higher activity for J77 and J70.

Magnetic: MSIS-86 least variance.

Residuals more negative with increasing activity near equator for all

but MSIS-86 and more positive with increasing activity near poles

for MSIS-77, J77, J70. Coverage to Ap 160.

Day/year: MSIS-77 least variance.Residuals have no clear trend.

Longitude/UT: MSIS least variance.

Residuals more positive near magnetic poles for J70.

Comments: Little overall difference between models except Jacchia

models slightly worse in latitude variations.

MSIS-86 trends: altitude.

85r

Page 90: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 130-200FIO.?: 70-110

Parameter: Total DensitySource: AE-C MESA Accel.

Dates: 73353-75100

Data File: MESA-C

Best quiet mean: .00 (J70)

Best quiet SD: .15 (MSIS-77)Best active mean: .07 (JTO)

Best active SD: .15 (MSIS-77)

Worst quiet mean: .11 (MSIS-86,-83

Worst quiet SD: .18 (J77,J70)Worst active mean: .14 (MSIS-86)

Worst active SD: .21 (J77)

Altitude: MSIS-83 J70 least variance.

Residuals more positive with decreasing altitude for MSIS models.

Latitude: MSIS least variance.

Residuals more positive toward north for MSIS models and more positive

toward both poles for for J77 and J70.

Local Time: MSIS least variance.

Residuals have diurnal variation for J77 and J70.

Mean FI0.7: MSIS least variance.

Residuals more positive with increasing activity for J70.

Delta FI0.7: MSIS-83 MSIS-77 least variance.

Residuals more positive with increasing activity for all models.

Coverage small.

Magnetic: MSIS least variance.Residuals near equator are irregular and near poles more positive with

higher activity for all models. Coverage to Ap 100 near equator

and Ap 130 near pole.

Day/year: MSIS-?7 least variance.

Longitude/UT: Variances similar for all models except worse for J77.

Comments: Jacchia models better than MSIS in absolute values but slightlyworse in standard deviations. Jacchia models worse for latitude

and daily variations.

MSIS-86 trends: latitude, delta FI0.7.

86

Page 91: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-250 Parameter: Total DensityFI0.7:70-110 Source: AE-CMESAAccel.

Best quiet mean: .02 (MSIS-86)Best quiet SD: .21 (all)Best active mean: .02 (MSIS-86)Best active SD: .20 (MSIS-77)

Altitude: All models have low variance.Residuals flat for all models.

Latitude: MSIS-86 least variance.Residuals flat but irregular for all models.

Dates_ 73353-76110Data File: MESA-C

Worst quiet mean: -.08 (MSIS-77)

Worst quiet SD: .21Worst active mean: .07 (J77)

Worst active SD: .23 (J77)

Local Time: MSIS-77 least variance.

Residuals have semidiurnal variation for all but MSIS-77.

Mean FIO.7: J77 least variance.

No obvious trends.

Delta FI0.7: MSIS-77 J77 least variance.

Residuals more positive with increasing activity for all models.

Magnetic: MSIS-77 least variance.

Residuals irregular. Coverage to Ap 130.

Day/year: J70 least variance.No obvious trends.

Longitude/UT: All models have low variance.

Comments: Little overall difference between models but Jacchia models

worse for daily variation and J77 worse for latitude variation.

MSIS-86 trends: delta FIO.7.

87

Page 92: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 130-200 Parameter: Total Density Dates: 74001-75100FI0.7:70-110 Source: AE-C OSS MS Data File: OSSC48

Best quiet mean: -.O1 (MSIS-86,-83) Worst quiet mean: -.07 (J70)

Best quiet SD: .10 (MSIS-77) Worst quiet SD: .13 (J77,J70)Best active mean: .00 (MSIS-77) Worst active mean:-.02 (J70)

Best active SD: .11 (MSIS-77) Worst active SD: .16 (J77)

Altitude: MSIS-77ieast variance.

Residuals more positive with increasing altitude for J77.

Latitude: MSIS least variance.

Residuals more positive toward north for MSIS models and more positive

toward both poles for for J77 and J70.

Local Time: MSIS least variance.

Residuals have diurnal variation for J77 and J70.

Mean FI0.7: MSIS-77 least variance.

No obvious trend.

Delta FI0.7: MSIS-77 J77 least variance.

Residuals more positive with increasing activity for all models.

Coverage small.

Magnetic: MSIS-77 least variance.

Residuals near equator are more negative with higher activity for

J77 and J70. Coverage to Ap 130.

Day/year: MSIS-77 least variance.

Longitude/UT: MSIS least variance.

Co,_nents: Little overall difference between models but Jacchia models

worse for latitude and daily variations.

MSIS-86 trends: latitude, delta FI0.7.

88

Page 93: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-390FI0.7:70-110

Parameter: Total DensitySource: AE-C OSS MS

Best quiet mean: .01 (J70)

Best quiet SD: .14 (MSIS)Best active mean: .00 (J70)

Best active SD: .15 (MSIS-86)

Dates: 74001-76161

Data File: OSSC2OOS20

Worst quiet mean: .09 (J77)

Worst quiet SD: .16 (J70)

Worst active mean: .10 (MSIS-83)

Worst active SD: .19 (J77)

Altitude: MSIS-86, -83 least variance.

Residuals more negative at higher altitudes for all models.

Latitude: MSIS-83 least variance.

Residuals more positive near the equator for all models.

Local Time: MSIS least variance.

Residuals have terdiurnal variation for J77.

Mean FI0.7: MSIS-86 least variance.

No obvious trends.

Delta FI0.7: MSIS-77 J70 least variance.

Residuals more positive with increasing activity for MSIS-86, -83,and J70.

Magnetic: MSIS-83 least variance.

Residuals irregular. Coverage to Ap 130.

Day/year: MSIS-83 least variance.No obvious trends.

Longitude/UT: All models have low variance.

Comments: Little overall difference between models but Jacchia models

worse for daily variation J77 worse for latitude variation.

MSIS-86 trends: altitude, latitude, and delta FI0.7.

89

Page 94: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 130-200

FI0.7:70-80

Parameter: Total DensitySource: AE-D MESA Accel.

Dates: 75284-76029

Data File: MESA-D

Best quiet mean: .00 (MSIS-83,-77) Worst quiet mean: -.03 (MSIS-86)

Best quiet SD: .14 (MSIS-77,J70) Worst quiet SD: .15 (MSIS-86,-83,J77)Best active mean: .00 (MSIS-83) Worst active mean: .04 (MSIS-77)

Best active SD: .15 (all but J77) Worst active SD: .17 (J77)

Altitude: Jacchia least variance.

Residuals more negative with decreasing altitude for MSIS models.

Latitude: J70 least variance.

Residuals flat except more positive toward south for J77.

Local Time: MSIS-86 JTO least variance.

Residuals flat but irregular.

Mean FI0.7: InsuffiCient coverage.

Delta FI0.7: J77 J70 least variance.

Residuals more positive with increasing activity for all models.

Coverage small.

Magnetic: MSIS least variance.

Residuals flat near equator and more positivewith higher activity for

all models. Coverage to Ap 50 near equator and Ap 70 near pole.

Day/year: Insufficient coverage.

Longitude/UT: Variances similar for all models except worse for J77.

Residuals negative near south magnetic pole.

Comments: Little overall difference between models.

MSIS-86 trends: altitude, and magnetic activity.

9O

Page 95: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-250 Parameter: Total Density Dates: 75284-76029FIO.7:70-80 Source: AE-DMESAAccel. Data File: MESA-E

Best quiet mean: .01 (J77) Worst quiet mean: -.11 (MSIS-77)Best quiet SD: .18 (not MSIS-83) Worst quiet SD: .19 (MSIS-83)Best active mean: .03 (MSIS-83) Worst active mean:-.O8 (MSIS-86)Best active SD: .19 (not J77) Worst active SD: .20 (J77)

Altitude: All models have low variance.Residuals flat for all models.

Latitude: Variances similar for all models.Residuals flat but irregular for all models.

Local Time: Variances similar for all models.Residuals flat but irregular for all models.

MeanFI0.7: Insufficient coverage.

Delta FI0.7: J77 J70 least variance.Residuals more positive with increasing activity for all models.

Magnetic: Variances similar for all models.Residuals irregular. Coverage to Ap 50 near equator and Ap 70 nearpoles.

Day/year: Insufficient coverage.

Longitude/UT: All models have low variance.

Comments: Little overall difference between models.

MSIS-86 trends: delta FI0.7.

91

Page 96: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 130-200FI0.7:70-80

Best quiet mean: -.01 (MSIS,J70)

Best quiet SD: .11 (MSIS,J70)Best active mean: .00 (J70)

Best active SD: .13 (MSIS)

Altitude: Variances similar for all models.

Residuals flat for all models.

Parameter: Total DensitySource: AE-D OSS MS

Dates: 75291-76029

Data File: OSSD48

Worst quiet mean: .04 (J77)

Worst quiet SD: .13 (J77)

Worst active mean: .06 (MSIS-77,J77)

Worst active SD: .15 (J77)

Latitude: MSIS-77 least variance.

Residuals flat except more positive toward south for J77.

Local Time: Variances similar for all models.

Residuals flat but irregular.

Mean FI0.7: Insufficient coverage.

Delta FI0.7: All models have low variance.

Residuals flat for all models. Coverage small.

Magnetic: Variances similar for all models.

Residuals flat near equator and more positive with higher activity for

all models. Coverage to Ap 50 near equator and Ap 70 near pole.

Day/year: Insufficient coverage.

Longitude/UT: Variances similar for all models except worse for J77.Residuals more negative near magnetic poles for all models.

Comments: Little overall difference between models.

MSIS-86 trends: magnetic activity and longitude.

92

Page 97: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-390 Parameter: Total Density Dates: 75291-76029

FI0.7:70-80 Source: AE-D OSS MS Data File: OSSD48

Best quiet mean: -.02 (MSIS-83) Worst quiet mean: -.20 (MSIS-77)

Best quiet SD: .17 (MSIS-86,Jac) Worst quiet SD: .18 (MSIS-83,-77

Best active mean: .00 (MSIS-83) Worst active mean:-.12 (MSIS-77)

Best active SD: .21 (MSIS-86,J70) Worst active SD: .23 (J77)

Altitude: MSIS-83 J70 least variance.

Residuals flat for all models.

Latitude: MSIS-77 least variance.

Residuals more positive near equator for all models.

Local Time: MSIS-77 least variance.

Residuals flat but irregular for all models.

Mean FI0.7: Insufficient coverage.

Delta FI0.7: MSIS-77, J77 J70 least variance.

Residuals more positive with increasing activity for all models.

Magnetic: MSIS-83, -77 least variance.

Residuals irregular. Coverage to Ap 50 near equator and Ap 70 near

poles.

Day/year: Insufficient coverage.

Longitude/UT: MSIS-77 least variance.

Residuals more negativ e near magnetic poles.

Comments: Little overall difference between models except MSIS-77

worse.

MSIS-86 trends: delta FI0.7 and longitude.

93

Page 98: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-400FI0.7:70-200

Parameter: Total Density Dates: 75178-79021Source: Cactus Accel. Data File: CACTUSTENTH

Best quiet mean: -.03 (J77)

Best quiet SD: .14 (MSIS-86)Best active mean:-.02 (MSIS-86)

Best active SD: .17 (MSIS-86)

Worst quiet mean: -.26 (MSIS-77)

Worst quiet SD: .18 (MSIS-77)

Worst active mean:-.15 (MSIS-77)

Worst active SD: .21 (J77)

Altitude: J77 J70 least variance.

Residuals sharply negative below 270 km for MSIS-86 -83, more

negative with increasing altitude for MSIS-77, and rather flat for J70 andJ77.

Latitude: MSIS-86, -77, J70 least variance.

Residuals more positive near equator for MSIS-83 and more negative

near equator for J77. Coverage 30S to 3ON.

Local Time: MSIS-86 least variance.

Residuals have diurnal variation for all models.

Mean FI0.7: J77 J70 least variance.

Residuals irregular.

Delta FI0.7: J77 J70 least variance.

Residuals more positive with increasing activity for MSIS models.

Magnetic: MSIS-83 least variance.

Residuals irregularly more positive with increasing activity for all models.

Day/year: MSIS-86 -83 least variance.Residuals have semiannual variation with equinox minimum for all models.

Longitude/UT: All models have low varlance.

Comments: Little overall difference between models except MSIS-77

(significantly worse) and Jacchia models significantly worse forlocal timevariations.

MSIS-86 trends: altitude, mean and delta FI0.7, and magnetic activity.

94

Page 99: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 400-600FI0.7:70-200

Parameter: Total DensitySource: Cactus Accel.

Dates_ 75178-79021

Data File: CACTUSTENTH

Best quiet mean: -.01 (MSIS-83,J77) Worst quiet mean: -.36 (MSIS-77)

Best quiet SD: .24 (MSIS-86) Worst quiet SD: .28 (MSIS-77)

Best active mean: .00 (MSIS-86) Worst active mean:-.23 (MSIS-77)

Best active SD: .28 (MSIS-86) Worst active SD: .31 (J77)

Altitude: J70 least variance.

Residuals more positive with increasing altitude for all models.

Latitude: MSIS-77, J70 least variance.

Residuals more positive near equator for MSIS-86, -83, flat for

MSIS-77 J77, S shaped for J70. Coverage 30S to 3ON.

Local Time: MSIS-86 least variance.Residuals have semidiurnal variation for all models.

Mean FI0.7: J77 least variance.

Residuals irregular.

Delta FI0.7: MSIS-83 least variance.

Residuals irregularly more positive with increasing activity forMSIS models.

Magnetic: MSIS-83 least variance.Residuals irregularly more positive with increasing activity for all models.

Day/year: MSIS-86 -83 least variance.

Residuals have semiannual variation with equinox minimum for all models.

Longitude/UT: All models have low variance.

Comments: Little overall difference between models except MSIS-77

(significantly worse) and Jacchia models significantly worse forlocal time variations.

MSIS-86 trends altitude, delta FI0.7, and magnetic activity.

95

Page 100: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 130-200

FI0.7:70-80

Parameter: Total Density Dates: 75335-76320Source: AE-E MESA Accel. Data File: MESA-E

Best quiet mean: -.O1 (MSIS-77,J77) Worst quiet mean: -.03 (J70)

Best quiet SD: .12 (MSIS) Worst quiet SD: .14 (J77,J70)Best active mean:-.02 (J70) Worst active mean: .07 (MSIS-83)

Best active SD: .14 (MSIS-77) Worst active SD: .16 (J77)

Altitude: J77 least variance.

Residuals more positive with decreasing altitude for all models.

Latitude: All models have low variance.

Coverage 20S to 2ON.

Local Time: MSIS-86 least variance.Residuals have semidiurnal variation for all but MSIS-86.

Mean FI0.7: Insufficient coverage.

Delta FI0.7: MSIS least variance.

Residuals more negative with increasing activity for J77 andJ70 models.

Magnetic: MSIS least variance.

Residuals more positive at highest activity for all models.

to Ap 110.

Coverage

Day/year: MSIS-86 -83 least variance.

Residuals more negative in middle of year for all models.

Longitude/UT: All models have low variance.

Comments: Little overall difference between models although J70

and J77 significantly worse for diurnal, delta FI0.7 and magnetic

activity variations.

MSIS-86 trends: altitude.

96

Page 101: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 200-250FI0.7:70-110

Parameter: Total DensitySource: AE-E MESA Aeoel.

Best quiet mean: .00 (MSIS-83)

Best quiet SD: .18 (MSIS-86)Best active mean: .O1 (MSIS-77)

Best active SD: .17 (MSIS-86)

Altitude: MSIS-77 least variance.

Dates: 75335-77278

Data File: MESA-E

Worst quiet mean: -.06 (MSIS-77)

Worst quiet SD: .20 (J77,J70)Worst active mean: .05 (MSIS-83)

Worst active SD: .20 (J77)

Residuals more positive with increasing altitude for all models.

Latitude: All models have low variance.

Coverage 20S to 2ON.

Local Time: MSIS least variance.

Residuals have semidiurnal variation for all models.

Mean FI0.7: JTO least variance.

Residuals irregular for all models.

Delta FI0.7: MSIS least variance.

Residuals more negative with increasing activity for J77 and J70.

Magnetic: Variances similar for all models.

Residuals irregular. Coverage to Ap 110.

Day/year: MSIS-86 -83 least variance.Residuals have no clear trend.

Longitude/UT: All models have low variance.

Comments: Little overall difference between models although J70

and J77 significantly worse for diurnal, and delta FI0.7 variations.

MSIS-86 trends: altitude, local time.

97

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Altitude: 130-200 Parameter: Total Density Dates: 75343-76319

FI0.7:70-80 Source: AE-E OSS MS Data File: OSS-E

Best quiet mean: .00 (MSIS-83) Worst quiet mean: -.07 (MSIS-77,JTO)

Best quiet SD: .13 (MSIS-77) Worst quiet SD: .17 (JTO)

Best active mean: .02 (MSIS-86,-83) Worst active mean:-.11 (J77)

Best active SD: .15 (MSIS-83,-77 Worst active SD: .19 (J77)

Altitude: J77 least variance.

Residuals more positive with decreasing altitude for all models.

Latitude: All models have low variance.

Coverage 20S to 2ON.

Local Time: MSIS-86 least variance.

Residuals have semidiurnal variation for MSIS-77, J77, and JTO.

Mean FI0.7: Insufficient coverage.

Delta FI0.7: MSIS least variance.

Residuals more negative with increasing activity for MSIS-77, J77 and

JTO models.

Magnetic: MSIS-77 J77 least variance.Residuals more positive with increasing activity for all models. Coverage

to Ap 110.

Day/year: MSIS-77 least variance.

Residuals have no clear trend.

Longitude/UT: All models have low variance.

Comments: MSIS models slightly better overall than the Jacchia models,

but Jacchia models significantly worse for local time variations.

MSIS-86 trends: altitude and magnetic activity.

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Altitude : 200-400FI0.7:70-170

Parameter: Total DensitySource: AE-E OSS MS

Dates: 75343-78336

Data File: OSS-E

Best quiet mean: -.O1 (J77) Worst quiet mean: -.15 (MSIS-77)

Best quiet SD: .18 (MSIS-83) Worst quiet SD: .21 (MSIS-77,J70)

Best active mean:-.03 (MSIS-86,-83) Worst active mean:-.12 (MSIS-77)

Best active SD: .19 (MSIS-86) Worst active SD: .23 (J77)

Altitude: MSIS-83 least variance.

Residuals more negative with increasing altitude for MSIS-77

J70.

Latitude: All models have low variance.

Coverage 20S to 2ON.

Local Time: MSIS-86 least variance.

Residuals have semidiurnal variation for all models and diurnal

for J77 and J70.

Mean FI0.7: All models same variance.

Residuals flat for all models.

Delta FI0.7: MSIS least variance.

Residuals more negative with increasing activity for J77 and J70.

Magnetic: J77 MSIS-77 least variance.

Residuals more positive at highest activity for all models.

to Ap 110.

Coverage

Day/year: MSIS-83 J70 least variance.Residuals have no clear trend.

Longitude/UT: All models have low variance.

Comments: Little Overall difference between models except

MSIS-77 (worse), but Jacchia models significantly worse forlocal time and delta FI0.7 variations.

MSIS-86 trends: altitude, local time, and magnetic activity.

Page 104: High Altitude Atmospheric Modeling - NASA · High Altitude Atmospheric Modeling Alan E. Hedin Laboratory for Atmospheres Goddard Space Flight Center Greenbelt, Maryland National Aeronautics

Altitude: 130-200FIO.7:70-80

Parameter: Total DensitySource: AE-E NACE MS

Dates: 75341-76307

Data File: NACE-E

Best quiet mean: -.O5 (all but J70) Worst quiet mean: -.07 (JTO)

Best quiet SD: .11 (MSIS-86) Worst quiet SD: .17 (J77)

Best active mean:-.04 (MSIS-86,-83) Worst active mean:-.15 (J77)

Best active SD: .13 (MSIS-86,-83 Worst active SD: .19 (J77)

Altitude: MSIS-86,-83 least variance_

Residuals more negative with decreasing altitude for all models.

Latitude: MSIS-86 least variance.

Residuals more positive in northern hemisphere for J70.

Coverage 2OS to 2ON.

Local Time: MSIS-86 least variance.

Residuals have semidiurnal variation for MSIS-77, J77, J70.

Mean FI0.7: Insufficient coverage.

Delta FIO.7: MSIS-86,-83 least variance.

Residuals more negative with increasing activity for MSIS-77 andJ77 models.

Magnetic: MSIS-86, -83 least variance.

Residuals flat but irregular for all models except more negative

with increasing activity for J77. coverage to Ap 150.

Day/year: MSIS-86 -83 least variance.Residuals have annual variation with June minimum for MSIS-77, J77,

and J70 models.

Longitude/UT: All models have low variance.

Comments: MSIS models better than Jacchia models overall. Jacchia models

significantly worse for local time variations and annual.

MSIS-86 trends: altitude.

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Altitude: 200-400

FI0.7:70-230

Parameter: Total DensitySource: AE-E NACE MS

Dates; 75341-81155

Data File: NACE-E

Best quiet mean: -.07 (J70)

Best quiet SD: .19 (MSIS-83)Best active mean:-.07 (MSIS-83)

Best active SD: .22 (MSIS-83)

Worst quiet mean: -.22 (MSIS-77)

Worst quiet SD: .23 (MSIS-77)Worst active mean:-.18 (MSIS-77)

Worst active SD: .24 (MSIS-77)

Altitude: J70 least variance.

Residuals more negative with increasing altitude for MSIS.

Latitude: All models have low variance.

Coverage 20S to 2ON.

Local Time: MSIS-86 least variance.Residuals have semidiurnal variation for all models and diurnal

for J77 and J70.

Mean FI0.7: MSIS-86 least variance.

Residuals irregularly more negative with increasing activity for MSIS

models and flat for J70 and J77.

Delta FI0.7: J70 least variance.

Residuals flat but irregular for all models.

Magnetic: J77 MSIS-77 least variance.

Residuals irregularly more positive for all models. Coverage to Ap 150.

Day/year: J77 J70 least variance.Residuals have semiannual variation with equinox minimum for all models.

Longitude/UT: All models have low variance.

Comments: Little overall difference between models except

MSIS-77 (worse) but Jacchia models worse for local time variations.

MSIS-86 trends: altitude, local time, mean FIO.7, annual, and magnetic

activity.

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Altitude: 400-480

FI0.7:160-230Parameter: Total DensitySource:AE-E NACE MS

Dates: 78336-80281

Data File: NACE-E

Best quiet mean: -.08 (J70) Worst quiet mean: -.32 (MSIS-77)

Best quiet SD: .18 (J77) Worst quiet SD: .22 (MSIS-77)

Best active mean:-.14 (J77,J70) Worst active mean:-.29 (MSIS-77)Best active SD: .23 (not MSIS-77) Worst active SD: .27 (MSIS-77)

Altitude: J70 least variance.

Residuals flat except morepositive with increasing altitude forMSIS-77 models.

Latitude: All models have low variance.

Coverage 20S to 2ON.

Local Time: MSIS-86,-83, J77 least variance.

Residuals have semidiurnal variation for all models except terdiurnal

for J77.

Mean FI0.7: MSIS-86,-83 least variance.

Residuals more negative with increasing activity except for MSIS-83.

Delta FI0.7: MSIS-86,-83 least variance.

Residuals flat but irregular for all models.

Magnetic: J77 least variance.

Residuals flat but irregular for all models. Coverage to Ap 150.

Day/year: All models the same except MSIS-77 worse.

Residuals irregular for all models.

LOngitude/UT: All models have low variance.

Comments: Little overall difference between models except MSIS-77 (worse).

MSIS-86 trends: local time mean FI0.7.

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Altitude: 200-400

FI0.7:125-230

Parameter: Total DensitySource: DE-B NACS MS

Dates: 81220-83047

Data File: NACSBRHOFIFTH

Best quiet mean: -.15 (J77)Best quiet SD: .14 (MSIS-86)

Best active mean:-.15 (MSIS-83)

Best active SD: .16 (MSIS-86)

Worst quiet mean: -.33 (MSIS-77)

Worst quiet SD: .23 (MSIS-77)Worst active mean:-.35 (MSIS-77)

Worst active SD: .21 (MSIS-77)

Altitude: MSIS least variance.

Residuals more negative at lowest altitude for all models.

Latitude: MSIS-86 least variance.

Residuals more negative near poles for MSIS083 and J70, and more

positive for J77. MSIS-77 more negative at south pole and positive

at north pole.

Local Time: MSIS-86 -83 least variance.

Residuals have semidiurnal or terdiurnal variation for MSIS-77,

J77 and J70.

Mean FI0.7: MSIS-86 -83 least variance.

Residuals more negative at higher activity for MSIS-77.

Delta FI0.7: MSIS-86 -83 least variance.

Residuals more negative at lowest activity for all models.

Magnetic: MSIS-86 least variance.

Residuals more negative with increasing activity for MSIS-83 and

-77 near pole. Coverage to Ap 200.

Day/year: MSIS-86 -83 least variance.Residuals have semiannual variation for all models.

Longitude/UT: MSIS-86 -83 least variance.Residuals more negative near magnetic poles for MSIS-77, J77, and

J70.

Comments: MSIS-86 model best for standard deviations and J77 best

for absolute values. Instrument calibration may be inaccurate.

MSIS-86 trends: altitude, delta FI0.7 and annual.

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Altitude: 400-800

FI0.7:150-230

Parameter: Total DensitySource: DE-B NACS MS

Best quiet mean: -.09 (J77)

Best quiet SD: .17 (MSIS-86)Best active mean:-.03 (J77)

Best active SD: .24 (MSIS-86)

Altitude: MSIS-86 least variance.

Dates: 81228-83014

Data File: NACSBRHOFIFTH

Worst quiet mean: -.38 (MSIS-77)

Worst quiet SD: .22 (MSIS-77)Worst active mean:-.31 (MSIS-77)

Worst active SD: .28 (MSIS-77)

Residuals more positive at higher altitudes for all models.

Latitude: MSIS'86 J70 least variance.

Residuals more positive at midlatitudes for J77.

Local Time: Variances similar for all models.

Residuals have semidlurnal or terdlurnal variation for all models.

Mean FI0.7: MSIS-86 least variance.

Residuals more positive at higher activity for all models.

Delta FI0.7: MSIS-86 least variance.

Residuals more negative at lowest activity for all models.

Magnetic: MSIS-86 least variance.

Residuals flat but irregular for all models. Coverage to Ap 200.

Day/year: MSIS-86 least variance.

Residuals have no clear trend. Coverage inadequate.

Longitude/UT: MSIS-86 J70 least variance.Residuals more negative near magnetic poles for all but MSIS-86.

Comments: MSIS and Jacchia models equivalent except MSIS-77 worse.

Instrument calibration may be inaccurate.

MSIS-86 trends: altitude, mean and delta FI0.7.

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NAS NalO_aiAeronauTcsandSoaceAcJrn_sI_aT_n

Report Documentation Page

I. Report No.

NASA TM 100707

2, Government Accession No.

4. Title and Subtitle

High Altitude Atmospheric Modeling

7. Author(s)

Alan E. Hedin

9. Performing Organization Name and Address

Laboratoryfor Atmospheres

Goddard Space Flight Center

Greenbelt, MD 20771

12. Sponsoring Agency Name and Address

National Aeronautics and Space Administration

washington, DC 20546-1000

15. Supplementary Notes

3. Recipient's Catalog No.

5. Report Date

October 1988

6. Performing Organization Code

614

8. Performing Organization Report No.

88B0260

10. Work Unit No.

11. Contract or Grant No.

13. Type of Report and Period Covered

Technical Memorandum

14. Sponsoring Agency Code

Sponsored .under USAF MIPR FY 616870485

16. Abstract

Five empirical models were compared with 13 data sets, including both atmospheric

drag-based data and mass spectrometer data. The most recently published model,

MSIS-86, was found to be the best model overall with an accuracy around 15 percent.

The excellent overall agreement of the mass spectrometer-based MSIS models with

the drag data, including both the older data from orbital decay and the newer

accelerometer data, suggests that the absolute calibration of the (ensemble of)

mass spectrometers and the assumed drag coefficient in the atomic oxygen regime

are consistent:tof5 pereent.

This study illustrates a number of the reasons for the current accuracy limit such

as calibration accuracy and unmodeled trends. Nevertheless, the largest variations

in total density in the thermosphere are accounted for, to a very high degree, by

existing models. The greatest potential for improvements is in areas where we

still have insufficient data (lik4 the lower thermosphere or exosphere), where

there are disagreements in technique (suc h as theexosphere) which can be resolved,

or wherever generally more accurate measurements become available.

17. Key Words(SuggestedbyAuthor(s))

Upper Atmosphere Structure

Thermospheric Density

18. Distribution Statement

Unclassified-Unlimited

Subject Category 46

19. Secur_ Classif. (of this report)

Unclassified

20. Securiw Classif.(ofthispage)

Unclassified

21. No. of pages 22. Price

NASA FORM 1_6 OCT

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