DocumentCode
810516
Title
Invariant poles feedback control of flexible highly variable spacecraft
Author
Mendel, J.
Author_Institution
McDonnell Douglas Astronautics Company, Huntington Beach, CA, USA
Volume
17
Issue
6
fYear
1972
fDate
12/1/1972 12:00:00 AM
Firstpage
814
Lastpage
821
Abstract
This paper describes a technique for single-axis control of a model of a highly flexible Space Station. Active damping of lower frequency flexibility modes is employed. In the control technique, referred to as invariant poles feedback control (IPFC), feedback gains are adjusted so that the closed-loop system characteristic.
Keywords
Adaptive control; Pole assignment; Space-vehicle control; Actuators; Control systems; Damping; Equations; Feedback control; Filtering; Frequency; NASA; Space stations; Space vehicles;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1972.1100161
Filename
1100161
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