一种满足空地导弹发射角的航路规划研究  

A Route Planning Algorithm Satisfying Air-to-Ground Missile's Emission Angle

作　　者：轩永波[1] 黄长强[1] 陈中起[1] 

机构地区：[1]空军工程大学工程学院,西安710038

出　　处：《电光与控制》2009年第4期38-41,共4页Electronics Optics & Control

基　　金：军队重点科研基金资助项目(HX05205)

摘　　要：针对战机实施对地巡航导弹投放的航路规划中解决飞机的进入角约束问题,提出了一种遗传算法获得初始航路规划方法;在此基础上运用B样条曲线理论进行航路光顺获得二次航路规划,解决了飞机到达目标区发射空地导弹时导弹发射角限制问题。仿真结果表明,该算法既满足飞机过载要求,又满足导弹发射角要求,可有效提高飞机的任务成功率。Considering the limit to entry angle of aircraft in the route planning for launching air-to-ground cruise missiles, a traditional genetic algorithm was used to get an initial route planning method. Then the theory of Bezier spline to smooth the above route planning for obtaining the 2nd route planning, the limited emission angle problem of air-to-ground missile was solved. Simulation results showed that the method can satisfying both the overloading requirement of aircraft and the requirement to emission angle of missile, which can greatly improve the task survival probability of the aircraft.

关 键 词：航路规划 遗传算法 航路光顺 作战使用 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计]