刚体卫星姿态PID控制，在有无干扰及飞轮失效情况下的仿真-PID control of rigid satellite attitude of actuator for flywheel

描述刚体卫星姿态稳定控制的程序。分为三种情况，小推力控制，飞轮控制与小推力飞轮联合控制。能在干扰下稳定卫星的姿态。- The program of attitude stabilization control for rigid satellite. It is divided into three situations: small thrust control, flywheel control and small thrust flywheel combined control.