Rate-Profiler Based Minimum-Time Control for Spacecraft Attitude Manoeuver-Reference-Cited by-同舟云学术

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Rate-Profiler Based Minimum-Time Control for Spacecraft Attitude Manoeuver

Published:2001-09 Issue:15 Volume:34 Page:53-60
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Saitoh Tetsu,Maeda Ken,Ninomiya Keiken,Hashimoto Tatsuaki

Publisher

Elsevier BV

Subject

General Medicine

Reference16 articles.

1. Optimal nonlinear feedback control for spacecraft attitude maneuvers;Carrington;Journal of Guidance, Control, and Dynamics,1986

2. Attitude determination and control of Clementine during lunar mapping;Creamer;Journal of Guidance, Control, and Dynamics,1996

3. Generalized results for precision attitude reference systems using gyros;Farrenkopf,1974

4. Inorbit alignment and scale-factor calibration of gyroscopes on board HALCA spacecraft;Hashimoto,1998

5. Robust time-optimal control of uncertain flexible spacecraft;Liu;Journal of Guidance, Control, and Dynamics,1992

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