火力与指挥控制Issue(11)：157-159,163,4.
基于遗传算法的反导拦截弹助推段自动驾驶仪的设计
Boost Phase Autopilot Design of Anti-missile Interceptor Using Genetic Algorithm
堵会晓 1黄靓1
作者信息
- 1. 平顶山工业职业技术学院，河南 平顶山 467001
- 折叠
摘要
Abstract
The anti-missile interceptor usually does not execute large overall maneuvering flight, and the trajectory is flat in the boost phase. The small disturbance linearized equations are used to design the three-loop autopilot,including the damping loop,the angle of attack loop,and the overload loop. Characteristic points are chosen based on ideal trajectory. The missile model is simplified as a second order one on each characteristic point. Since lots of parametes in different control loops are to be optimized,it is difficult to use the general optimization method. Here we use genetic algorighm to optimize the controller parameters. The simulation results show that the proposed scheme can track the command signals exactly.关键词
反导拦截弹/遗传算法/自动驾驶仪Key words
anti-missile interceptor/genetic algorithm/autopilot分类
军事科技引用本文复制引用
堵会晓,黄靓..基于遗传算法的反导拦截弹助推段自动驾驶仪的设计[J].火力与指挥控制,2014,(11):157-159,163,4.
