discrete reaching law method 离散趋近律方法
The formula of anticipant control moment is deduced by adopting the method of exponent reaching law and twitter reducing of boundary layer.
并研究了姿控发动机的配置特点和点火逻辑，给出了由期望力矩计算实际控制力矩的方法。
The sliding surface is designed by the "pole-placement" method and the variable structure control is determined by the "reaching law approach".
采用极点配置方法设计滑模面，基于趋近律方法求取变结构控制律。
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