简易控制超音速火箭靶弹方案最优制导律设计  

Optimal Programmed Guidance Law Design of Simple Control Supersonic Rocket Target

作　　者：沈冠军[1] 冯顺山[2] 曹红松[1] 

机构地区：[1]中北大学机电工程学院,山西太原030051 [2]北京理工大学爆炸科学与技术国家重点实验室,北京100081

出　　处：《北京理工大学学报》2015年第3期256-261,共6页Transactions of Beijing Institute of Technology

基　　金：国家部委支撑基金资助项目(62201070503)

摘　　要：针对简易控制超音速火箭靶弹方案供靶弹道设计问题,提出了一种基于粒子群方法和Gauss伪谱法相结合的火箭靶弹供靶最优制导律设计方法.该方法首先在爬升-拉平段,利用粒子群方法优化得出火箭靶弹在拉平段具有最大动能的最优射角和爬升段最优起控时间,然后利用Gauss伪谱法设计得出平飞供靶段最优控制律.仿真结果表明,该方法能够快速获得最优方案供靶弹道和方案制导律,并且可以较好地满足供靶指标,为火箭靶弹供靶弹道设计提供参考.Aiming at the project trajectory design problem for target of simple control supersonic rocket target,an optimal guidance law design method of rocket target was proposed base on the particle swarm optimization and Gauss pseudo-spectral method.First,according to the rocket target has the greatest kinetic energy at the beginning of leveled segment,the optimal incident angle and control moment were calculated by using the particle swarm optimization during the climb-leveled segment.Then,the optimal level flight guidance law was calculated based on Gauss pseudo-spectral method.Simulation results show that,using the method proposed,the optimal project trajectory and guidance law can be obtained quickly,as well as the indicators for target can be met well.The method can provide a reference for trajectory design of rocket target.

关 键 词：最优制导律 超音速火箭靶弹 简易控制 方案弹道 

分 类 号：TJ013.2[兵器科学与技术—兵器发射理论与技术]