| 逆系统空空导弹控制器设计(英文) |
| |
| 引用本文： | 何素娟,周凤岐.逆系统空空导弹控制器设计(英文)[J].火力与指挥控制,2011,8(8). |
| |
| 作者姓名： | 何素娟 周凤岐 |
| |
| 作者单位： | 西北工业大学精确制导与控制研究所,西安,710072 |
| |
| 基金项目： | 国家自然科学基金; 教育部新世纪人才支持计划基金资助项目 |
| |
| 摘 要： | 利用非线性控制的逆系统方法,设计了导弹质心运动动力学系统的控制器。该控制器通过对弹道坐标系下导弹的切向过载和法向过载的控制,使导弹在控制系统中的速度、弹道倾角和弹道偏角输出信息渐近跟踪制导指令,以实现空空导弹对攻击目标的打击。仿真结果表明,导弹的质心运动参数以较高的精度快速跟踪制导指令,系统性能良好。
|
| 关 键 词： | 逆系统 空空导弹 动力学系统 渐近无差跟踪 |
Design of Controller Based on Inverse System for Air-to-Air Missile |
| |
| HE Su-juan,ZHOU Feng-qi.Design of Controller Based on Inverse System for Air-to-Air Missile[J].Fire Control & Command Control,2011,8(8). |
| |
| Authors: | HE Su-juan ZHOU Feng-qi |
| |
| Institution: | HE Su-juan,ZHOU Feng-qi(Institute of Precision Guidance and Control,Northwestern Polytechnical University,Xi'an 710072,China) |
| |
| Abstract: | Using the inverse system method in nonlinear control,a controller is designed for a missile dynamics system of the centroid motion.In order to realize the attack of the target,the output information of the control system including velocity,trajectory inclination and declination can track the guidance command through the control of the tangential and normal overloading of the missile in the trajectory coordinate.Simulation results show that the centroid motion parameters can quickly track the guidance comman... |
| |
| Keywords: | inverse system air-to-air missile dynamics system no error progressive tracking |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
