求翻译：针对俯仰平面内导弹制导控制一体化的非线性动力学系统具有非匹配不确定项情况，结合反演控制，自适应控制和滑模控制方法，设计了一种导弹自适应反演滑模控制器。反演设计每一步采用自适应算法对不确定性的上界进行估计，为了避免传统反演自适应算法中的“计算膨胀”问题，并没有采用滤波器对虚拟控制输入的导数进行估计，而是将虚拟控制量的导数作为不缺定性处理，利用自适应滑模控制的鲁棒性对其进行补偿，简化了控制系统的设计。采用Lyapunov稳定性理论证明了系统的稳定性。数值验证了该算法的有效性。是什么意思？

With a non- matching uncertainties , combined with inversion control, adaptive control and sliding mode control method to design a missile Adaptive backstepping sliding mode controller for missile guidance control in the pitch plane integration of nonlinear dynamical systems

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The missile guidance control integration non-linear dynamics system has the non-match indefinite situation in view of the pitching plane in, the union inversion control, the adaptive control and the slip form control method, has designed one kind of missile auto-adapted inversion slip form controlle

Pitching plane integrated missile guidance and control for nonlinear systems with mismatched uncertainties, combined with inversion of control, adaptive control and sliding mode control approach, design a missile Adaptive backstepping sliding mode controller. Anti-played design each step used since

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