机动弹头激光末制导姿态控制系统设计  

Attitude Control System for Laser Terminal Guided Maneuver Warhead

作　　者：闵海波[1] 王仕成[1] 邓方林[1] 郭英然[1] 

机构地区：[1]第二炮兵工程学院,西安710025

出　　处：《航天控制》2006年第4期13-17,56,共6页Aerospace Control

摘　　要：简要分析了机动弹头激光末制导的必要性和可行性。针对机动弹头再入弹道和制导方式的特殊性,分析了激光末制导机动弹头姿控系统设计的关键技术。通过与传统控制方案的对比,提出指令前馈和变结构反馈的复合控制方案。仿真结果表明,系统具有较好的鲁棒性,能够基本满足系统姿态控制设计要求。The necessity and feasibility for the application of laser-terminal-guidance technique in maneuver warhead is briefly presented. In view of the particularity for maneuver warhead reentry trajectory and the guidance method, key techniques in attitude control system design are analyzed. Comparing with the tradi- tional control scheme, an integrated control approach based on the instruction feed-forward control plus variable structure feed-back control technique is put forward. Simulation result indicates that this scheme has relatively high robustness and satisfies the design requirement.

关 键 词：机动弹头 指令前馈 变结构控制 激光末制导 

分 类 号：V448.22[航空宇航科学与技术—飞行器设计]