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
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;
Conference_Titel :
American Control Conference, 1989
Conference_Location :
Pittsburgh, PA, USA
