DocumentCode
487888
Title
Rational Fraction Approach and Attitude Control of Spinning Satellite using Gyrotorquer
Author
De, Prasanta K. ; Iyer, Ashok
Author_Institution
Department of Computer Science and Electrical Engineering, University of Nevada, Las Vegas, NV 89154
fYear
1989
fDate
21-23 June 1989
Firstpage
1579
Lastpage
1584
Abstract
The problem of joint stabilization and tracking of a spinning satellite system in addition to its regulation are considered. Rational Fractional approach is used to obtain coprime equations in a multivariate setting. Parameterized compensators are obtained for regulation and, simultaneous stabilization and tracking cases. Simulation results are presented to show the accomplishment of attitude control in different settings with simple control inputs.
Keywords
Constraint optimization; Control systems; Design optimization; Feedback; Flywheels; Satellites; Spinning; System performance; Torque control; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1989
Conference_Location
Pittsburgh, PA, USA
Type
conf
Filename
4790439
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