巡航导弹航向规避弹道的优化设计

航向规避弹道的设计可视为一个多约束的优化问题。对此，通过选择导弹到达每个航路点的时间，用两点约束问题代替多点约束问题，得出了控制能量最优解，并分析了弹道特性。计算结果表明，弹道曲线在不超出导弹可用过载的前提下，通过所有航路点，并满足落点要求。该方法可用于航迹规划研究。

Optimum Design of Heading Avoidance Trajectory for Cruise Missile

As one part of route planning,the design of heading avoidance trajectory plays an important role in improving the fighting efficiency of cruise missile.This paper presents a new method to design the heading avoidance trajetory. The design of heading avoidance trajectory is a very complicated multipoint constained optimization problem.We altered the problem with a simple two points constained optimization problem by selecting the time when the missile arrives at the waypoint.The results of trajectory calculation shown in table 1,figure 2 proved the method worked well.