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George Mason University
Sensor Management ina Sensor Rich Environment
Carl G. Schaefer, Jr.Kenneth J. Hintz
Department of Electrical and Computer Engineeringand
Center of Excellence in C3IGeorge Mason University, Fairfax, VA 22030
SPIE AeroSense24 – 28 April 2000
Orlando, FL
April 25, 2000 SPIE Aerosense 2000 2
George Mason University
The Sensor Rich Environment
• Sensor rich environment (SRE) – large network of inexpensive, unimodal, passive sensors with the ability to capture data in parallel.
• Contrast with C3I sensor environments – limited number of expensive, multimodal, and active sensors.
• Examples:– U.S. Navy DD-21 destroyer -- ~ 200,000 sensors.
– Aircraft health and usage monitoring systems (HUMS) – ~ 2,000 sensors.
– Others include networked building energy systems, autonomous space probes, satellite constellations, power grids, and others.
April 25, 2000 SPIE Aerosense 2000 3
George Mason University
The Sensor Rich Environment (cont’d)
• Overwhelming volume of data– One example: SH-60 HUMS
– 450 healthy aircraft 3 – 9 terabytes of data per month, 400 terabytes of data in 10 years
– Overabundance of data compounded when components fail.
• This is a “data rich, information poor (DRIP)” environment, especially at the human interface.
• In an SRE, system state estimation not constrained by sensors, but by network bandwidth, processor performance, human-machine interface.
April 25, 2000 SPIE Aerosense 2000 4
George Mason University
The Sensor Rich Environment (cont’d)
• Paradigm must change:– From: merely collecting vast amounts of data to
be analyzed later– To: determining information needs first,
followed by collection of only that data that can satisfy those needs.
April 25, 2000 SPIE Aerosense 2000 5
George Mason University
Characteristics of Sensor Rich Environments
• Large numbers of sensors and pseudosensors.• Massively distributed.• Tightly coupled.• Unimodal sensors (typically).• Stationary, perhaps overlapping, sensing or surveillance
volumes.• Fixed (non-agile and stationary) sensors.• (Relatively) inexpensive sensors.• Passive, rather than active, sensors.• Sensor type diversity.• Continuous and concurrent data acquisition.
April 25, 2000 SPIE Aerosense 2000 6
George Mason University
Helicopter HUMS Sensor Distribution
Aircraft Subsystem No. of Sensors or Pseudosensors
Aircraft States and Controls 158 Engines 344 Auxiliary Power Unit (APU) 7 Main Gearbox 29
Auxiliary Gearbox 59 Auxiliary Systems 12 Intermediate Gearbox 37 Tail Rotor Gearbox 31 Drive shafts/Hanger Bearings 84 Flight Regimes 202 Rotor Track and Balance 179 Hydraulics and Lubricants 134 External Loads 26 Fuel System 47 HUMS Status and Self-Test 304 Engine Nose Gearbox 26 Swashplate 13
April 25, 2000 SPIE Aerosense 2000 7
George Mason University
Helicopter HUMS Sensors
• Highly distributed sensor network– 1,700 sensors spread over 17 aircraft subsystems
• Single sensors covering multiple subsystems or performing multiple functions.– Accelerometer(s) at aircraft center of gravity
– Flight regime recognition, flight control system, load limiting device, aircraft vibration control, rotor track and balance.
• Tightly coupled sensor network. Significant data sharing and interaction between subsystems.
• Overlapping sensor volumes for gearbox fault monitoring.
April 25, 2000 SPIE Aerosense 2000 8
George Mason University
Distributed Sensing on Helicopter Tail Rotor Driveshaft
Individual Sensor
Pseudosensor
April 25, 2000 SPIE Aerosense 2000 9
George Mason University
GMU Comprehensive Sensor Manager
DataBase
Sensors
HumanOperator
SENSOR MANAGER
SensorScheduler(OGUPSA)
InformationInstantiator
MissionManager
Sen
sor
Sta
tus
INFORMATION SPACE
Mea
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men
t Req
uest
ObservationRequest
RequestRejection
Info
rmat
ion
Req
uest
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Info
rmat
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Req
uest
Wei
ghts
/P
riorit
y
Mission Goals/Objectives (offline) Real-time
requests
Measurementto
Observation
Observationto
Information
FUSION SPACE
Measure-ment
Order of BattleIntel EstimatesEnemy Doctrine
Wpn Characteristics
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Fusion Space
Mission Manager
Information Instantiator
Sensor Scheduler
Sensors
Human Operator
April 25, 2000 SPIE Aerosense 2000 10
George Mason University
Sensor Management for SRE’s• The GMU Comprehensive Sensor Management model can
be adapted to SRE without major architectural or functional changes.
• Architectural options;– Fully distributed.
• Issues relative to coordination of mission goals amongst distributed sensor managers.
– Fully centralized.• Issues concerning the immense size of the Applicable Function
Tables and Applicable Sensor Tables.
– Hybrid system• Distributed sensor schedulers partitioned along functional or
subsystem boundaries.• Single Mission Manager.
April 25, 2000 SPIE Aerosense 2000 13
George Mason University
Implications of Hybrid SM Architecture
• Difficulty in modeling faults and coupled failure modes may require local intelligence at each sensor.
• This implies an “interrupt driven” process, however, this is still consistent with the architecture of the original SM model.
• Meta-scheduler to coordinate subsystem sensor schedulers.• Use of intelligent sensors must be balanced against global
context in which system is situated.– True system or component failure?, or– Combat maneuvering?
• Information span – abstracting view of local data by placing it within the global context until it “makes sense”.
April 25, 2000 SPIE Aerosense 2000 14
George Mason University
Conclusions
• The GMU Comprehensive Sensor Management Model can be adapted to a sensor rich environment with only minor implementation changes.
• Research areas:– Mission Manager – adaptive goal lattices to compensate for real-time
reprioritization of mission needs.– Information Instantiator/Sensor Scheduler – methods to efficiently map
information needs to multiple and overlapping functional needs and to map these functional needs to sensors allocated to distributed sensor schedulers.
– Sensor Scheduler – development of an efficient meta-scheduler for coordinating multiple distributed sensor schedulers.
– Mission Manager – methods for abstracting local information and placing that information within the global context; the “information span”.
– Fusion Space – failure state estimators, data association techniques for the hybrid SM model.