Rational Fraction Approach and Attitude Control of Spinning Satellite Using Gyrotorquer
Document Type
Conference Proceeding
Publication Date
6-21-1989
Publication Title
American Control Conference, 1989
Publisher
IEEE
First page number:
1579
Last page number:
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
Artificial satellites – Attitude control systems; Artificial satellites – Control systems; Artificial satellites – Rotation; Constraint optimization; Control systems; Design optimization; Feedback; Flywheels; Satellites; Spinning; System performance; Torque control; Vehicles
Disciplines
Computer Engineering | Controls and Control Theory | Electrical and Computer Engineering | Engineering | Navigation, Guidance, Control and Dynamics
Language
English
Permissions
Use Find in Your Library, contact the author, or interlibrary loan to garner a copy of the item. Publisher policy does not allow archiving the final published version. If a post-print (author's peer-reviewed manuscript) is allowed and available, or publisher policy changes, the item will be deposited.
Repository Citation
De, P. K.,
Iyer, A.
(1989).
Rational Fraction Approach and Attitude Control of Spinning Satellite Using Gyrotorquer.
American Control Conference, 1989
1579-1584.
IEEE.