基于奇异最优控制的弹道导弹最大上升高度的推力控制问题研究

Thrust Control Problems of Maximum Lifting Height of the Ballistic Missile Based on Singular Optimal Control

对弹道导弹升空的动力学模型加入角度分析和模型优化,并用奇异最优控制的方法对一类非线性模型所产生的奇异弧和奇异球平面方程求解,从而得到弹道导弹的最优非线性反馈率.

Adding to angle analysis and optimization in the dynamic model of ballistic missile launch,singular arc and singular ball plane equations which is generated from a class of nonlinear models were solved by using singular optimal control. The optimal nonlinear feedback law of ballistic missile was obtained.