Flexible Spacecraft Control Design Using Pole Allocation Technique-Reference-Cited by-同舟云学术

Flexible Spacecraft Control Design Using Pole Allocation Technique

Published:1978-07 Issue:4 Volume:1 Page:279-281
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference9 articles.

1. Multiloop Analysis of a Precision Pointing Spacecraft with Controlled Flexible Appendages

2. 3Larson, V. and Likins, P.W. "An Application of Modern Control Theory to An Elastic Spacecraft," ESA Symposium on Dynamics and Contol of Non-Rigid Space Vehicles, Frascati-Roma, Italy, May24-26,1976.

3. 4Tracy, T.G. and Tseng, G.T. "Application of Quadratic Cost Optimal Control Theory to a Complex Flexible Spacecraft." AIAA Symposium on Dynamics and Control of Large Flexible Spacecraft, Blacksburg, Va., June13-15,1977.

4. On pole assignment in linear systems with incomplete state feedback

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