挠性卫星实验装置的全物理控制实验研究

Experiment Research For Physical Control of Flexible Satellite Experimental Instrument

针对常用的“飞轮一喷气”执行机构模式，采用ＰＩＤ控制和变结构控制方案，对挠性卫 星实验装置进行了小角度和大角度机动控制的全物理控制实验，取得令人满意的试验结果．

According to the 'wheel-thruster' actuator mode that is commonly used in satellite control, PID control scheme and variable structure control scheme are used in the physical control experiment, which is made on the flexible satellite experimental instrument, for the small and large angle maneuver control of the satellite. The results of the experiment are satisfied.