To eliminate the chattering of variable structure control ( VSC) in missile servo system for attitude control, the control law was expanded from second-order to n order on the basis of status trace and variable plane included angle.
为消除导弹姿态控制伺服系统变结构控制中的抖振,在状态轨迹与滑动平面夹角变结构控制律的基础上,将原来的二阶系统扩展为n阶。
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