防空导弹垂直发射的最优化控制研究

Research on the Optimal Control of the Vertical Launching Anti-aircraft Missile

在分析防空导弹垂直发射对制导控制系统的要求后，应用最优控制理论的方法。建立垂直发射初制导的数学模型，对初制导的方案进行设计，主要目的是按所要求的终端条件。按最优控制规律实现垂直发射后全方位转弯控制，并与中制导（末制导）的平稳交班。

After analyzing the requirement of the vertical launching for the control and guidance of anti-aircraft missile, the thesis applies the optimal control method and builds the mathematic model of vertical launching for the control and guidance of anti-aircraft missile. Finally, the project of initial guidance and control is designed in order to achieve the turn in all direction in vertical launching and handover with the intermediate （terminal） guidance smoothly.