Pitch/yaw momentum position control of roll momentum biased satellite system

In this paper, we utilize the roll momentum bias to control the pitch/yaw attitude of the satellite. While the previous control approaches have used the PD control approach, we design a new PID controller in order to improve the transient response over the existing methods. Through the example, we show that our control approach indeed improves the control performance over the existing results. For simulation, the system parameters are taken from the values of KOREASAT1.