气动/推力矢量飞行器分阶段复合控制分配策略设计

Journal of Systems Engineering and Electronics ›› 2013, Vol. 35 ›› Issue (6): 1249-1255.

气动/推力矢量飞行器分阶段复合控制分配策略设计

高峰¹，唐胜景¹，郭杰¹，师娇²

1. 飞行器动力学与控制教育部重点实验室，北京理工大学宇航学院，北京 100081；
2. 中国运载火箭技术研究院，北京 100076

收稿日期:2012-05-15 修回日期:2013-01-19 出版日期:2013-06-15 发布日期:2013-04-09

Compound control allocation strategy design of dual aero/ thrust vector flight vehicle based on different flight phases

GAO Feng ¹，TANG Sheng-jing ¹，GUO Jie ¹，SHI Jiao ²

1. Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace
Engineering, Beijing Institute of Technology, Beijing 100081, China;
2. China Academy of Launch Vehicle Technology, Beijing 100076, China

Received:2012-05-15 Revised:2013-01-19 Online:2013-06-15 Published:2013-04-09

摘要/Abstract

摘要：

以气动/燃气舵推力矢量复合控制反坦克导弹为研究对象，研究了不同飞行阶段下的气动/推力矢量复合控制分配策略问题。通过分析气动舵和燃气舵控制效率受导弹飞行速度变化的影响，并结合不同飞行阶段的飞行任务和特点，分别基于模糊逻辑以及链式递增理论，设计了适用于初始飞行段和末制导段的复合控制分配策略。仿真结果表明，设计的两种策略均保证了复合控制系统具有较快的响应速度和良好的控制精度，同时缩短了燃气舵的工作时间，减少了推力损失。

Abstract:

The compound control allocation strategy is mainly researched based on anti-tank missile with dual aero/jet vane thrust vector control. According to analyze the influence of
velocity on control efficiency of aerodynamic rudder and jet vane, and combine the analysis with the objectives and characteristics of different flight phases, the allocation strategies of initial flight phase and terminal guidance phase are designed based on fuzzy logic and increasing chain theory, separately. Simulation shows that the strategies have a good effect on flight control, and loss of thrust can be decreased at the same time.

中图分类号:

10.3969/j.issn.1001-506X.2013.06.20

高峰，唐胜景，郭杰，师娇. 气动/推力矢量飞行器分阶段复合控制分配策略设计[J]. Journal of Systems Engineering and Electronics, 2013, 35(6): 1249-1255.

GAO Feng ，TANG Sheng-jing ，GUO Jie ，SHI Jiao . Compound control allocation strategy design of dual aero/ thrust vector flight vehicle based on different flight phases[J]. Journal of Systems Engineering and Electronics, 2013, 35(6): 1249-1255.