Rigid body equations of motion for modeling and control of spacecraft formations. Part 1: Absolute equations of motion-Reference-Cited by-同舟云学术

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Rigid body equations of motion for modeling and control of spacecraft formations. Part 1: Absolute equations of motion

Published:2004 Issue: Volume: Page:
ISSN:
Container-title:Proceedings of the 2004 American Control Conference
language:
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Author:

Ploen S.R.,Hadaegh F.Y.,Scharf D.P.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx5/9503/30159/01384478.pdf?arnumber=1384478

Cited by 11 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

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3. Twistor-based synchronous sliding mode control of spacecraft attitude and position;Chinese Journal of Aeronautics;2018-05

4. Modeling Flexible-Body Dynamics in Real-Time Robotic Systems used in Satellite Servicing Simulations;AIAA Modeling and Simulation Technologies (MST) Conference;2013-08-15

5. Relative motion coupled control based on dual quaternion;Aerospace Science and Technology;2013-03

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