文件名称:dynamic_control
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基于三轴航天器的姿态控制，按照实际情况，充分考虑了三轴的动力学和运动学耦合，能够单独控制各个角度姿态-Based on three-axis attitude control of the spacecraft, according to the actual situation, fully taking into account the dynamic and kinematic coupling triaxial, can be controlled separately for each angular pose
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下载文件列表
dynamic_control\control.m
...............\kinematics.m
...............\yuhndongxue.mdl
dynamic_control