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Redundancy management of inertial systems.The paper reviews developments in failure detection and isolation techniques applicable to gimballed and strapdown systems. It examines basic redundancy management goals of improved reliability, performance and logistic costs, and explores mechanizations available for both input and output data handling. The meaning of redundant system reliability in terms of available coverage, system MTBF, and mission time is presented and the practical hardware performance limitations of failure detection and isolation techniques are explored. Simulation results are presented illustrating implementation coverages attainable considering IMU performance models and mission detection threshold requirements. The implications of a complete GN&C redundancy management method on inertial techniques are also explored.
Document ID
19730057167
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mckern, R. A.
Musoff, H.
(MIT Cambridge, Mass., United States)
Date Acquired
August 7, 2013
Publication Date
August 1, 1973
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 73-852
Meeting Information
Meeting: Guidance and Control Conference
Location: Key Biscayne, FL
Start Date: August 20, 1973
End Date: August 22, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A41969
Funding Number(s)
CONTRACT_GRANT: NAS9-13207
CONTRACT_GRANT: NAS8-27624
CONTRACT_GRANT: NAS9-8242
Distribution Limits
Public
Copyright
Other

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