Title

Rational fraction approach and attitude control of spinning satellite using gyrotorquer

Document Type

Conference Proceeding

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.

Disciplines

Computer Engineering | Controls and Control Theory | Electrical and Computer Engineering | Engineering | Navigation, Guidance, Control and Dynamics

Permissions

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