飞航导弹分层滑动模控制

LAYERED SLIDING MODEL CONTROL OF THE AERODYNAMIC MISSILE

对 １ 个二层的非线性模型进行了仿射型化，使块对角结构具有分层仿射型特点，提出了滑动模块对角控制器的设计方法，实现了飞航导弹的非线性控制系统的设计。仿真结果表明，这种设计方法对模型参数变化具有很强的鲁棒性。

The model of the areodynamic missile can be described as a block diagonal construction with four layers.After getting an affine form of 1 st and 2 nd layers,an affine form with four layers of the missile is gotten in this paper.By using the form , this paper develops a procedure called sliding model block diagonal controller , which realizes a design of a nonlinear system of a missile. The simulation shows that the procedure has a powerful robustness for the model.