初始优化轨道实时计算的拟牛顿法——防空导弹轨道优化的实时计算方法之一

Real-time computation of initial optimization trajectory with quasi-Newton methods:real-time computation methods of air defence missile trajectory′s optimization

提出防空导弹轨道优化的一些实时计算问题,并且应用拟牛顿法计算初始优化轨道。

Some real-time computation problems for the optimization of air defence missile trajectory are presented,and the quasi-Newton methods are used to compute the initial optimization trajectory.