Approximate algorithms for fast optimal attitude computationFast accurate algorithms are presented for computing an optimal attitude which minimizes a quadratic loss function. These algorithms compute an optimal rotation which carries a set of reference vectors into a set of corresponding observation vectors. Simplifications of these algorithms are obtained for the case of small rotation angles. Applications to the Magsat mission are discussed.
Document ID
19780066260
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Shuster, M. D. (Computer Sciences Corp. System Sciences Div., Silver Spring, Md., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking