大气层内的动能拦截器末制导段，为了提高对目标未知逃逸机动的鲁棒性，可采用变结构制导律。
During the terminal guidance phase of the kinetic kill vehicle in the atmosphere, the variable structure guidance law can be used to improve the robustness to unknown escaping maneuver of the target.
简要介绍了变结构控制理论和导弹制导律，对基于变结构控制的导弹制导律进行了比较详细的研究。
The theory of variable structure control and guidance laws of missiles is simply introduced. The guidance laws based on variable structure control are researched in detail.
应用变结构控制理论，引入模糊规则自适应地调整趋近律，设计了制导律。
Fuzzy logic rules are introduced to adjust approaching law adaptively, and the guidance is designed by applying variable structure control theory.
研究表明，由于变结构控制的应用，使得制导律具有很强的鲁棒性，比传统的比例导引律有更多的优越性。
Research shows because of the application of variable structure control, the guidance laws have strong robustness and more advantages over the conventional proportional navigation...
研究表明，由于变结构控制的应用，使得制导律具有很强的鲁棒性，比传统的比例导引律有更多的优越性。
Research shows because of the application of variable structure control, the guidance laws have strong robustness and more advantages over the conventional proportional navigation...
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