Title

Stable Fraction Approach and Attitude-control of a Spinning Satellite Using a Gyrotorquer

Document Type

Article

Publication Date

3-1992

Publication Title

International Journal of Systems Science

Volume

23

First page number:

311

Last page number:

328

Abstract

The problem of joint stabilization and tracking of a spinning satellite system in addition to its regulation are considered. The rational fractional approach is used to obtain coprime equations in a multivariate setting for both coupled and decoupled models. Parametrized compensators are obtained for regulation and stabilization with 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; Gyroscopes; Signal processing

Disciplines

Electrical and Computer Engineering | Power and Energy | Signal Processing | Systems and Communications

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.

Identifier

DOI: 10.1080/00207729208949209

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