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Attitude determination and parameter estimation using vector observations - TheoryProcedures for attitude determination based on Wahba's loss function are generalized to include the estimation of parameters other than the attitude, such as sensor biases. Optimization with respect to the attitude is carried out using the q-method, which does not require an a priori estimate of the attitude. Optimization with respect to the other parameters employs an iterative approach, which does require an a priori estimate of these parameters. Conventional state estimation methods require a priori estimates of both the parameters and the attitude, while the algorithm presented in this paper always computes the exact optimal attitude for given values of the parameters. Expressions for the covariance of the attitude and parameter estimates are derived.
Document ID
19890060352
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Markley, F. Landis
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 14, 2013
Publication Date
March 1, 1989
Publication Information
Publication: Journal of the Astronautical Sciences
Volume: 37
ISSN: 0021-9142
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
89A47723
Distribution Limits
Public
Copyright
Other

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