Reduced-Attitude Boresight Guidance and Control on Spacecraft for Pointing, Tracking, and Searching
A guidance and a control law are developed to maneuver the boresight axis of a spacecraft relative to a reference vector, using knowledge of the reference vector and the angular rates of the spacecraft. Therefore, this can be used in cases when the full attitude is not known or when the angle of the...
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Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2015-06, Vol.38 (6), p.1027-1035 |
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Format: | Artikel |
Sprache: | eng |
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