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以具有大面积太阳帆板的卫星大角度机动为背景，针对常用的“飞轮—喷气”执行机构模式研究了变结构控制方案，考虑了控制精度和喷气消耗量问题，并成功地进行了国内首次挠性卫星大角度机动控制的全物理仿真实验，取得了显著的效果。
Based on the large-scale satellite maneuvering with large-area solar panels, the variable-structure control scheme is studied for the commonly used “flywheel-jet” actuator mode, the control accuracy and jet consumption are considered, and the first time in China Full-physics simulation experiments of flexible satellite large-angle maneuvering have achieved remarkable results.