Time optimal slewing of flexible spacecraft-Reference-Cited by-同舟云学术

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Time optimal slewing of flexible spacecraft

Published:1987-12 Issue: Volume: Page:
ISSN:
Container-title:26th IEEE Conference on Decision and Control
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Author:

Ben-Asher Joseph,Burns John,Cliff Eugene

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx5/4049207/4049208/04049322.pdf?arnumber=4049322

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Frequency and Time Domain Analysis of an Aeroelastic Wing Multiple Component Structure;Numerical Functional Analysis and Optimization;2015-07

2. Simple Adaptive Control Applications to Large Flexible Structures;Journal of Guidance, Control, and Dynamics;2011-11

3. Minimum-time control characteristics of flexible structures;Journal of Guidance, Control, and Dynamics;1996-01

4. Minimum time pulse response based control of flexible structures;Journal of Guidance, Control, and Dynamics;1993-09

5. Optimal slewing of flexible spacecraft with prescribed sensitivity of terminal control;Guidance, Navigation and Control Conference;1993-08-09

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