一种变后掠翼导弹弹道快速优化方法  

Method of Rapid Trajectory Optimization for Missile with Morphing Swept Wings

作　　者：赵日[1] 孙瑞胜[1] 

机构地区：[1]南京理工大学能源与动力工程学院,南京210094

出　　处：《四川兵工学报》2014年第3期41-44,共4页Journal of Sichuan Ordnance

基　　金：国家自然科学基金(11176012);航空科学基金(20110159001)

摘　　要：变后掠翼导弹弹道优化问题是一个复杂的多变量优化问题;为了获得变后掠翼导弹飞行弹道,利用Radau伪谱法求解了同时满足路径约束和终端约束条件下的射程最远弹道轨迹;选取后掠角和攻角作为优化控制变量,并通过采取一系列实时性保证策略提高算法的计算效率;仿真结果表明:该方法能够快速优化出满足性能指标和约束条件的弹道轨迹;研究结果可为变后掠翼导弹在线重构的实现提供有益参考。Trajectory optimizing problem of missile with morphing swept wings was a complicated multi variable optimizing problem. To obtain the flight trajectory for missile with morphing swept wings, the radau pesudospectral method（RPM） was used to solve the flight trajectory with maximum range, satisfying both path constrains and terminal constrains. The sweep angle and attack angle was chosen as optimal con trol variables, and several strategies can ensure its realtime performance was adopted to improve the com pute efficiency. The simulation results indicate that RPM can solve the flight trajectory optimizing problem of missile with morphing swept wings quickly to satisfy the above optimization index and constraint condi tions. The results can provide a reference to the online trajectory reconfiguration of missile with morphing swept wings.

关 键 词：导弹 变后掠翼 弹道优化 Radau伪谱法 

分 类 号：TJ761.6[兵器科学与技术—武器系统与运用工程]