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Design of a TF Controller for Aerodynamic Missile Using Dynamic Inversion Sliding Mode Theory

机译：使用动态反转滑模理论设计空气动力导弹TF控制器的设计

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According to singular perturbations theory, this paper adopted aerodynamic missile layered control algorithm, and divided terrain following controller into three layers, that is, velocity layer, attitude angles layer and angular velocities one. A dynamic inversion sliding mode control algorithm was proposed for the design of aerodynamic missile terrain following controller, at the same time the uncertain errors of missile system were adequately considered to guarantee the tracking errors converge exponentially. Finally nonlinear six-degree-of freedom simulations of one aerodynamic missile were done, from the results it can be seen that the missile can follow the terrain configuration accurately, and the simulation results also showed that the designed system had strong robustness and rapidly tracking capability
机译：根据奇异的扰动理论，本文采用了空气动力导弹分层控制算法，并将地形划分为三层，即速度层，姿态角层和角速度。提出了一种动态反转滑模控制算法，为控制器的空气动力导弹地形设计，同时，导弹系统的不确定误差被充分考虑为保证跟踪误差呈指数汇总。最后是非线性的六程度自由模拟一个空气动力导弹，从结果可以看出，导弹可以准确遵循地形配置，并且模拟结果也表明设计的系统具有强大的鲁棒性和快速跟踪能力

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