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PID Controller Design for the Satellite Attitude Control System | ||
| Journal of Engineering | ||
| Article 1, Volume 15, Issue 1, 2009, Pages 3312-3320 | ||
| Author | ||
| Sami Kadhim Hasan Ar-Ramahi | ||
| Abstract | ||
| A PID controller satellite attitude yaw-axis control system was designed to step the angle of the satellite body via actuating a precise angular position of a DC motor as quickly and accurately as most optimally possible. The (PID) controller was advantageously chosen for its quick transient response and zero steady-state error. A mathematical model has been derived for the whole satellite attitude yaw-axis control system. Then, the computation power of the MATLAB is utilized to obtain a generalized optimal controller design that enables the satellite attitude yaw-axis control system to have the quickest settling time without excessive overshoot and zero steady state error. | ||
| Keywords | ||
| PID controller; ACS mathematical model; satellite attitude yaw; axis control system; ACS | ||
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