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An adaptive technique for a redundant-sensor navigation system.An on-line adaptive technique is developed to provide a self-contained redundant-sensor navigation system with a capability to utilize its full potentiality in reliability and performance. This adaptive system is structured as a multistage stochastic process of detection, identification, and compensation. It is shown that the detection system can be effectively constructed on the basis of a design value, specified by mission requirements, of the unknown parameter in the actual system, and of a degradation mode in the form of a constant bias jump. A suboptimal detection system on the basis of Wald's sequential analysis is developed using the concept of information value and information feedback. The developed system is easily implemented, and demonstrates a performance remarkably close to that of the optimal nonlinear detection system. An invariant transformation is derived to eliminate the effect of nuisance parameters such that the ambiguous identification system can be reduced to a set of disjoint simple hypotheses tests. By application of a technique of decoupled bias estimation in the compensation system the adaptive system can be operated without any complicated reorganization.
Document ID
19720055468
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chien, T.-T.
(MIT Cambridge, Mass., United States)
Date Acquired
August 6, 2013
Publication Date
August 1, 1972
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 72-863
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Guidance and Control Conference
Location: Stanford, CA
Start Date: August 14, 1972
End Date: August 16, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A39134
Funding Number(s)
CONTRACT_GRANT: NAS9-8242
Distribution Limits
Public
Copyright
Other

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