Kerpler's 1619 Ellipse Law Historical Mistake

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    Keplers 1619 third law historical mistakeIs: There is no planetary motion around the Sun

    All objects move in an absolute circular orbit and objects in the sameneighborhood cause a planetary system ellipsis Illusions

    Figure - 1

    r

    Sun

    Mercury

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    Kepler Third law is: F = a/T2 = k/a2 and said there is planetary motion around the SunAnd it is an ellipse with the Sun at the focus of the ellipse?Since Kepler was a GermanNewton changed the letter a to the letter r for an English brand!

    Newton Second law is: F =r/ t2 = k/r2 and said there is planetary motion around the SuAstronomers found that planetary motion around the Sun is not an ellipse but a rotatingellipseEinstein rigged physics with time travel law r/t2 = k/ r2 + k1/r4 to describe a rotating elli

    7 billion people were/are told by Alfred Nobel prize winner physicists that Planets rotatearound the Sun in a rotating ellipseWhat if I can prove them all wrong?That there is no Suns Planets and Moons! But there are objects with absolute motion ofcircle and the relative motion is an visual ellipse and match experimental dataI am Joe NahhasAnd I am after Alfred Nobel Institution head

    Sun

    Mercur

    y

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    Newton gave the equation of the ellipse:As: r (, t) = [a (1-)/ (1+ cosine )]Einstein said he corrected Newton and wrote the new equation:

    Is: r (, t) = a (1-)/ [1+ cosine ( - )]

    Page 2It is a fact that Astronomers see this axis tilt and Einstein got a formula forit: = {6 G M/a c (1 - )} [180/ ] [36526/T (days)][3600]G = 6.673 x 10-11= gravitational acceleration constantM =2x1030kg = mass of the SunEccentricity of Mercurys orbit = = 0.206T= 88 days = period of Planet mercurys rotation around the Sun

    And c = 299792.458 km/sec =light speed/secAnd a = 58.2 x 106 km/sec = semi major axis of planet Mercury orbit

    = {6 () 6.673 x 10-11 (2 x 1030)/58.2 x 106 (299792.458) [1 (0.206)]} x[180/ ] [36526/88] [3600] = 43 seconds of an arc per century

    Newton used magical powers or action at a distanceforce F = G m M/r2

    Einstein said if Newton can add magical power then Ican do magic powers of Newton and add Einsteinsown magical powers of time travel force and the forceIs F = G m M/r2 (space force) + k/r4 (time force)

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    These two Magicians claim that what we see is due tomagic where the Sun is pulling on the planets to keepthem around? Did anyone see the Sun Pulling?Did anyone see a robe from the Sun pulling on planets

    to keep them around? Page 3

    What is modern physics?

    Did anyone hear the big bang? Did anyone saw a black hole? Did anyone find Einsteins

    gravity waves? Did anyone hook up a hose to the sky and funnel dark energy to verify E= mc2? Does anyone have a proof of Newtons action at a distance? Does anyone have a

    proof of Einstein time travel? Does anyone figure out why humans have to accept Alfred

    Nobel prize winners nuclear claims that the universe is made up of particles that dies andrebirth billion billion times a second? Hey dude I am a redneck one grandfather was a

    damn farmer and my other grandfather was a damn Carpenter and my father was a muchdamn redneck I sometimes feel reluctant to claim him but I never knew what a dumb assreally is till I met my science teacher talking about the greatest idiots of physics starting

    With the seven idiots in order Copernicus Galileo Newton and Einstein!

    Newtons space force: F = G m M/r2Einsteins Newton space - time:F = G m M/r2 (Newtons space force) + k/r4

    (Einsteins time force)The force is with Joe Nahhas and in real time space F = 0

    Nahhas said the only magic is an act of kindness of a human to all others!

    My act of kindness to humanity is to make humanity aware that there is nothing Nobel

    about Alfred Nobel Institution that changed physics to stupidity

    What I am saying is that there is no Newtonsgravitational force and Einsteins space time force issilly to say the least and I can prove that there is nogravitational force between the Sun and the Planetsforce, or, F = o solution is a rotating ellipse Illusion.To start with let me solve this equation F = 0. Thesolution of F = 0 is the equation of a real time circleIs r = r 0 e (+ t)All there is in the Universe is objects of mass m moving in space (x, y, z) ata location

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    r = r (x, y, z). The state of any object in the Universe can be expressedas the productS = m r; State = mass x location:P = d S/d t = m (d r/d t) + (dm/d t) r = Total moment

    = change of location + change of mass

    = m v + m' r; v = velocity = d r/d t; m' = mass change rateF = d P/d t = dS/dt = Total force= m (dr/dt) +2(dm/d t) (d r/d t) + (dm/dt) r= m + 2m'v +m" r; = acceleration; m'' = mass acceleration rate

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    In polar coordinates systemr = r r (1) ;v = r' r(1) + r ' (1) ; = (r" - r')r(1) + (2r'' + r ")(1)r = location; v = velocity; = accelerationF = m + 2m'v +m" r

    F = m [(r"-r') r (1) + (2r'' + r ") (1)]+2m'[r' r (1) + r ' (1)]+ (m" r) r (1)

    = [d (m r)/dt - (m r) '] r (1) + (1/m r) [d (mr')/d t] (1)= [-G m M/r] r (1) -------------------- Newton's Gravitational Law

    Proof:First r = r [cosine + sine ] = r r (1)Define r (1) = cosine + sine Define v = d r/d t = r' r (1) + r d[r (1)]/d t = r' r (1) + r'[- sine + cosine ]

    = r' r (1) + r ' (1)Define (1) = -sine +cosine ;And with r (1) = cosine + sine Then d [ (1)]/d t= ' [- cosine - sine = - ' r (1)And d [r (1)]/d t = ' [-sine + cosine ] = ' (1)Define = d [r' r (1) + r ' (1)] /d t

    = r" r (1) + r'd [r (1)]/d t + r' ' r (1) + r " r (1) +r 'd [ (1)]/d t = (r" - r') r (1) + (2r'' + r ") (1)With d (m r)/dt - (m r) ' = F (r)And d (mr')/d t = 0

    With m = constant, thenWith d r/dt - r ' = F (r) Eq-1And d (r')/d t = 0 Eq-2With d r/dt - r ' = 0 E q 1And d (r')/d t = 0 Eq-2From Eq-2: d (r')/d t = 0Then r' = h = constantDifferentiate with respect to time

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    Then 2rr'' + r" = 0Divide by r'Then 2(r'/r) + "/' = 0And 2(r'/r) = - "/' = 2[ (r) + (r)]Also, r = r0 (, 0) e [ (r) + (r)] t

    And ' = ' 0 (, 0) e -2[ (r) + (r)] tFor a fixed orbit: r = 0Also, r = r 0 (, 0)e t

    Page 5And ' = ' 0 (, 0) e -2 tWith d r/dt - r ' = 0Let u = 1/r; r = 1/u; r' = h = /uAnd d r/d t = (d r/ d u) (d u /d ) (d / d t) = (- 1/u ) () (d u/ d )

    = - h (d u/ d )

    And d r/ d t = - h () (d u/ d )= [- h/r] (d u/ d )= - h u (d u/ d )

    With d r/dt - r ' = 0 E q 1And - h u (d u/ d ) (1/u) (h u) = 0Then (d u/ d ) + u = 0

    Then u = A e - Then r 0 (, 0) = (1/A) e

    And r 0 (, 0) = r 0 (0, 0) e And r = r 0 (0, 0) e e t

    Or, r = r 0 e (+ t)What I am saying Dear Pope is this is the equation ofmotion of any planet!

    It is also the equation of motion of the smallestparticle light!

    Now Planet Mercury motion isr m = r m0 e [ (m)+ (m) t]

    The Sun Motion is r s = r s0 e [ (s)+ (s) t]

    Sun r r s Mercury

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    r1 r0 r mX1 r2

    X2Earth

    Page 6In mathematical form: r1= x1 + r sAnd r2 = x2 + r m

    Then r2 - r1 = x2 - x1 + r m r sOr, r = r0 + (r m r s)

    To find the extreme values of r,Then: d r/d t = d r0/d t+ (d r m/d t d r s/ d t) = 0

    And (d r m/d t d r s/ d t) = 0; d r0/d t = 0

    And d r m/d t = d r s/ d tNow Planet Mercury motion isr m = r m0 e [ (m)+ (m) t]

    The Sun Motion isr s = r s0 e [ (s)+ (s) t]

    Andd r m/d t = r m0 [ (m) + (m)]e [ (m)+ (m) t]And d r s/ d t = r s0 [ (s) + (s)]e [ (s)+ (s) t]

    Withr m0 [ (m) + (m)] Cosine [ (m) + (m) t]= r s0 [ (s) + (s)] Cosine [ (s) + (s) t]And r m0 [ (m) + (m)] sine [ (m) + (m) t]= r s0 [ (s) + (s)] sine [ (s) + (s) t]Then dividing we get: tan [ (n) + (n) t] = tan [ (s) + (s) t]

    Or,[ (m) + (m) t] = [ (s) + (s) t] + [n = 0; n =0]

    And (m) - (s) = space Illusion = [ (s) - (m)] t = real time delayThis is the time delay IllusionAnd, r m0 [ (m) + (m)]= r s0 [ (s) + (s)]And [ (s) + (s)] = (r m0 /r s0)[ (m) + (m)]

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    And[ (s) + (s)] -[ (m) + (m)] = [(r m0 /r s0) -1][ (m) + (m)]

    In arc second per century:

    Is: [ (s) + (s)] -[ (m) + (m)] x (180/) x (36526/88) x (3600)

    = [(r m0 /r s0) -1][ (m) + (m)] x (180/) x (36526/88) x (3600)

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    And,r m0 [ (m) + (m)]= r s0 [ (s) + (s)]

    And r m0 [ (m) + (m)] = r e0 [ (e) + (e)]

    And[ (s) + (s)] -[ (e) + (e)] = [(r m0 /r e0) -1][ (m) + (m)]

    In arc second per century:

    Is: [ (e) + (e)] -[ (m) + (m)] x (180/) x (36526/88) x (3600)

    = [(r m0 /r e0) -1][ (m) + (m)] x (180/) x (36526/88) x (3600) = 43

    r m0

    r s0M M M Mercury S Sun

    r m0 r 0

    Is: r 0= distance between centersIs: r max = r 0 +(r m0 + r s0)And r min = r 0 -(r m0 + r s0)And c = (r max - r min)/2 = r m0 + r s0And a = (r max + r min)/2 = r 0

    With c = (r max - r min)/2 = r m0 + r s0

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    And a = (r max + r min)/2 = r 0This establishes visual ellipse of semi major axis a and a semi minoraxis b = (a - c) = a [1 (c/a) ] = a (1 )And h = 2 a b = 2 a (1 )Areal Velocity is: 2 a (1 )/T

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    Figure - 1

    Page 9

    And Farthest distance = r max = r 0 +(r m0 + r s0) = a + c

    And closest distance = r min = r 0 -(r m0 + r s0) = a - c

    r

    Sun

    Mercury

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    At closest approach: h =2 a (1 )/TAnd dividing h / (a c) = 2 a (1 )/T a (1 ) Or r' = h will give ' (a) = 2 (1 )/T (1 )

    And for any motion ' = ' 0 (, 0) e -2 tAnd = {[cosine 2 t + sine 2 t] 1}' 0 (, 0)And = (x) + (y)

    = [cosine 2 t + sine 2 t] ' 0 (, 0)

    And (x) = [cosine 2 t] ' 0 (, 0)= [1 2 sine t] ' 0 (, 0)

    And (x) - ' (0) = - 2' 0 (, 0)sine t= -2(2) [ (1-)]/T (1-) ] sine t

    =- 4 [ (1-)]/T (1-) ] sine t

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    If this apsidal motion is to be found as visual effects, then

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    With, v = spin velocity; v* = orbital velocityAnd v/c = (v* + v)/c = tan t

    = -4 [ (1-)]/T (1-) ] sine {Inverse tan [(v* + v)/c]} radians

    Multiplication by 180/ to change to degrees

    = (-720/T) {[ (1-)]/ (1-) } sine {Inverse tan [(v* + v)/c]}DegreesAnd multiplication by 1 century = 36526 days and using T in days

    (calculated) = (-720x36526/T days) {[ (1-)]/ (1-) } xsine {Inverse tan [(v* + v)/c]} degrees/100 years

    And in arc seconds per century: (calculated) = (-720x36526x3600/T days) {[ (1-)]/ (1-) } x

    sine {Inverse tan [(v* + v)/c]} degrees/100 years = 43Page 11

    Sun

    Mercury

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    Is: [ (e) + (e)] -[ (m) + (m)] x (180/) x (36526/88) x (3600)

    = [(r m0 /r e0) -1][ (m) + (m)] x (180/) x (36526/88) x (3600) = 43

    And in arc seconds per century: (calculated) = (-720x36526x3600/T days) {[ (1-)]/ (1-) } x

    sine {Inverse tan [(v* + v)/c]} degrees/100 years = 43

    All rights reserved

    Is: [ (e) + (e)] -[ (m) + (m)] x (180/) x (36526/88) x (3600)

    = [(r m0 /r e0) -1][ (m) + (m)] x (180/) x (36526/88) x (3600) = 43

    And in arc seconds per century: (calculated) = (-720x36526x3600/T days) {[ (1-)]/ (1-) } x

    sine {Inverse tan [(v* + v)/c]} degrees/100 years = 43

    All rights reservedPage 12

    Pluto 5906.4 90730 4.74

    Planet Distance rX 106km

    PlanetOrbit T

    Orbitspeed vinkm/sec

    LessEarthspeed

    Spinspeedkm/sec

    Angular velocity;v/rarc sec/ century

    Mercury 58.2 88 47.9 18.1 .002 70.75Venus 108.2 224.7 35.05 5.7 6.52 10.86Earth 149.6 365.26 29.8 .46511 4.1Mars 227.936 687 24.14 0.2411Jupiter 778.412 4333 13.06 12.6

    Saturn 1,426.725 10760 9.65 9.87Uranus 2,870.97 30690 6.80 2.59Neptune 4,498 60180 5.43 2.68Pluto 5906.4 90730 4.74