Abstract
The characteristics of a special PID control (zero PID control), where the proportional gain is almost zero, are presented. On this basis, a design procedure of roll/yaw control of a bias momentum satellites is developed and shown by example. The roll/yaw control laws have been developed by many authors and these are usually non-minimum phase control. Comparisons are made with these control laws in terms of response, stability, and noise sensitivity. It was found that the characteristics of the zero PID control lie between the non-minimum phase control and the ordinary lead compensation and thus it is widely applicable to various circumstances.
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