导弹协同编队<i>H</i><sub>∞</sub>制导律设计 -- 西北工业大学学报,2017,35(5):767-773
论文:2017,Vol:35,Issue(5):767-773
引用本文:
黄伟, 徐建城, 吴佳斌, 吴华兴. 导弹协同编队H制导律设计[J]. 西北工业大学学报
Huang Wei, Xu Jiancheng, Wu Jiabin, Wu Huaxing. Design of H Guidance Law for Missile Cooperative Formation[J]. Northwestern polytechnical university

导弹协同编队H制导律设计
黄伟1, 徐建城1, 吴佳斌2, 吴华兴3
1. 西北工业大学 电子信息学院, 陕西 西安 710072;
2. 西北工业大学 自动化学院, 陕西 西安 710072;
3. 空军工程大学 航空航天工程学院, 陕西 西安 710038
摘要:
在导弹协同编队飞行过程中,为使从弹制导系统在满足干扰抑制指标要求的同时,具有良好的动态响应特性,提出一种基于H控制理论的比例积分制导律算法。在三维空间中建立新的领从弹相对运动方程,将领弹加速度信息视为有界扰动,以相对距离和从弹加速度作为状态量和控制量,得到从弹制导系统的状态方程。通过状态变换和系统增广,将从弹制导律设计问题转换为H控制问题,得到满足H性能指标的比例积分控制器,实现了导弹编队队形的生成、跟踪和保持。仿真结果验证了算法的有效性。
关键词:    导弹编队    比例积分控制器    鲁棒性    响应特性    制导律    角速度   
Design of H Guidance Law for Missile Cooperative Formation
Huang Wei1, Xu Jiancheng1, Wu Jiabin2, Wu Huaxing3
1. School of Electronic and Information, Northwestern Polytechnic University, Xi'an 710072, China;
2. School of Automation, Northwestern Polytechnic University, Xi'an 710072, China;
3. College of Aeronautics and Astronautics Engineering, Air Force Engineering University, Xi'an 710038, China
Abstract:
In the flight process of missile cooperative formation, to meet anti-interference performance and dynamic responsive characteristics of guiding system for following missiles, a proportion-integration guiding law based on H∞ control theory is proposed. By building new equation of relative motion between the leader and the follower in 3D space, considering the leader's acceleration as bounded disturbance, and taking relative range and the follower's acceleration as the state variable and control variable respectively, the state equation of the follower is derived. State transformation and system augmentation are used to transfer the guiding law design problem into H∞ control problem, and a proportion-integration controller meeting H∞ performance is presented, thus the generation, tracking and keeping of missile formation shape is implemented. Simulation results demonstrate the validity of the arithmetic.
Key words:    missile formation    proportion-integration controller    robustness    responsive characteristics    guidance law    angular velocity   
收稿日期: 2017-02-20     修回日期:
DOI:
基金项目: 国家自然科学基金(61472441)资助
通讯作者:     Email:
作者简介: 黄伟(1980-),西北工业大学博士研究生,主要从事先进成像制导与控制技术的研究。
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