Dynamic Feedback Linearization and Large Pitch Attitude Control of Satellite Using Solar Radiation Pressure
Document Type
Conference Proceeding
Publication Date
6-21-1995
Publication Title
Proceedings of the American Control Conference
Publisher
IEEE
Volume
5
First page number:
3131
Last page number:
3135
Abstract
The question of large angle pitch attitude maneuver of satellites using solar radiation pressure is considered. For pitch axis maneuver, two highly reflective control surfaces are used to generate radiation moment. Based on dynamic feedback linearization, a nonlinear control law is derived for large pitch attitude control. In the closed-loop system, the response characteristics of the pitch angle are governed by a fourth order linear differential equation. Robustness of control system is obtained by the integral error feedback. Simulation results are presented to show that in the closed-loop system, attitude control of the satellite is accomplished in spite of the parameter uncertainty in the system.
Keywords
Aerospace control; Artificial satellites; Attitude control; Feedback; Linearisation techniques; Radiation pressure; Solar radiation
Disciplines
Controls and Control Theory | Electrical and Computer Engineering | Engineering | 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.
Repository Citation
Singh, S. N.,
Yim, W.
(1995).
Dynamic Feedback Linearization and Large Pitch Attitude Control of Satellite Using Solar Radiation Pressure.
Proceedings of the American Control Conference, 5
3131-3135.
IEEE.