A signed switching time bang-bang attitude control law for fine pointing of flexible spacecraft†
Author:
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
http://www.tandfonline.com/doi/pdf/10.1080/00207178408933308
Reference1 articles.
1. Adaptive, high precision, satellite attitude control for microprocessor implementation
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4. Microsatellite Attitude Determination and Control Subsystem Design and Implementation: Software-in-the-Loop Approach;Mathematical Problems in Engineering;2014
5. Spacecraft vibration reduction using pulse-width pulse-frequency modulated input shaper;Guidance, Navigation, and Control Conference;1997-08-11
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