Research on Sliding Mode Control of FoldingWing Missile’s Lateral Overload
折叠翼导弹侧向过载的滑模变结构控制研究，杨亮，杨剑影，考虑折叠翼导弹在弹翼瞬间展开对数学模型变化的影响，且该瞬间过程比较复杂而且快速，我们将该过程简化模拟为模型参数的快速突变
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