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An Adaptive Technique for a Redundant-Sensor Navigation SystemAn 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. The gyro navigation system is modeled as a Gauss-Markov process, with degradation modes defined as changes in characteristics specified by parameters associated with the model. The adaptive system is formulated as a multistage stochastic process: (1) a detection system, (2) an identification system and (3) a compensation system. It is shown that the sufficient statistics for the partially observable process in the detection and identification system is the posterior measure of the state of degradation, conditioned on the measurement history.
Document ID
19750001970
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Chien, T. T.
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1972
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
T-560
NASA-CR-140313
Report Number: T-560
Report Number: NASA-CR-140313
Accession Number
75N10042
Funding Number(s)
CONTRACT_GRANT: NAS9-8242
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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