Determination of poles and zeros of transfer functions for flexible spacecraft attitude control†
Author:
Affiliation:
1. a National Aerospace Laboratory , 1880 Jindaiji-machi, Chofu, Tokyo, 182, Japan
2. b School of Engineering and Applied Science, University of California , Los Angeles, California, 90024, U.S.A
Publisher
Informa UK Limited
Subject
Computer Science Applications,Control and Systems Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/00207177608932803
Reference7 articles.
1. Poles, zeros, and feedback: State space interpretation
2. A computational method for finding the zeros of a multivariable linear time invariant system
3. Zeros determination in large-scale multivariable systems
4. KWAKERNAAK , H. , and SIVAN , R. , 1972 , Linear Optimal Control Systems ( Wiley- Interscience ), pp. 41, 42 .
5. LIKINS , P. W. , 1970 , Technical Report 32–1329 , Jet Propulsion Laboratory .
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1. Modal identities for multibody elastic spacecraft;Journal of Guidance, Control, and Dynamics;1991-03
2. The role of zeros in the performance of multiinput, multioutput feedback systems;IEEE Transactions on Education;1990
3. Research on system zeros: a survey;International Journal of Control;1989-10
4. Poles and transmission zeros of flexible spacecraft control systems;Journal of Guidance, Control, and Dynamics;1985-03
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