应用保护映射理论的高超声速飞行器自适应控制律设计

doi:10.7527/S1000-6893.2015.0030

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应用保护映射理论的高超声速飞行器自适应控制律设计

肖地波, 陆宇平, 刘燕斌, 许晨

南京航空航天大学航天学院, 南京 210016

收稿日期:2014-10-29 修回日期:2015-01-23 出版日期:2015-10-15 发布日期:2015-01-30
通讯作者: 刘燕斌, Tel.: 025-84896521-6206 E-mail: liuyb@nuaa.edu.cn E-mail:liuyb@nuaa.edu.cn
作者简介:肖地波男, 博士研究生。主要研究方向: 高超声速飞行器建模和控制。 E-mail: xiaodibo1986@163.com;陆宇平男, 教授, 博士生导师。主要研究方向: 先进飞行控制技术, 高超声速飞行技术, 变体飞行器控制。 E-mail: yplac@nuaa.edu.cn;刘燕斌男, 副教授。主要研究方向: 临近空间高超声速飞行控制, 飞行器复杂建模与控制。 Tel: 025-84896521-6206 E-mail: liuyb@nuaa.edu.cn;许晨男, 博士研究生。主要研究方向: 多刚体系统建模与控制。 E-mail: nuaaxuchen@126.com
基金资助:
国家自然科学基金 (61403191); 江苏省普通高校研究生科研创新计划资助项目 (CXZZ13_0169); 北航虚拟现实技术与系统国家重点实验室开放基金 (BUAA-VR-14KF-03)

Adaptive control law design using guardian maps theory for hypersonic vehicles

XIAO Dibo, LU Yuping, LIU Yanbin, XU Chen

College of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received:2014-10-29 Revised:2015-01-23 Online:2015-10-15 Published:2015-01-30
Supported by:
National Natural Science Foundation of China (61403191); Funding of Jiangsu Innovation Program for Graduate Education (CXZZ13_0169); The Open Funding Project of State Key Laboratory of Virtual Reality Technology and Systems (BUAA-VR-14KF-03)

摘要/Abstract

摘要：

针对高超声速飞行器包线范围广、参数变化大的控制需求,应用保护映射理论提出一种高超声速飞行器的自适应控制律设计方法。首先建立整个飞行包线内的线性变参数(LPV)模型,在参数变化边界点设计一个初始的控制结构和参数,然后基于保护映射理论分析初始控制结构使闭环系统稳定的参数范围,通过迭代自动获取整个包线内满足性能指标的控制参数,进而通过多项式拟合设计出高超声速飞行器自适应控制律。所提出的方法能够根据初始控制结构自动寻找一系列满足性能要求的控制器参数,并确定这些控制参数满足闭环系统稳定的设计范围。仿真结果表明,所设计的自适应控制律能够确保高超声速飞行器大包线的设计要求,实现闭环系统的鲁棒稳定。

关键词: 保护映射, 高超声速飞行器, 自适应控制, 线性变参数(LPV), 大包线控制

Abstract:

An adaptive control law design approach using the guardian maps theory is proposed for hypersonic vehicles over the control requirements of a broad flight envelope and wide parameter variation range. Firstly, a linear parameter varying (LPV) model throughout the whole flight envelope is established, and an initial controller structure and parameter are designed at the boundary of the parameters variation range. Secondly, the parameter change range of the initial controller structure is analyzed so as to ensure the system stability; furthermore, based on the guardian maps theory, the corresponding controller parameters can be automatically obtained in relation to the expected performance criterion over the whole flight envelope by the step-by-step iteration. Besides this, the complete adaptive control law is acquired with the integration of these obtained control parameters by applying the curve-fitting mean. The proposed method is able to automatically search a set of controller parameters meeting the performance criterion in the whole flight envelope according to the initial controller, and at the same time to determine the design range guaranteeing global stability of the closed-loop system. Simulation results show that the designed adaptive control law can drive this close system to reach the anticipated design requirements for hypersonic vehicles and also to ensure robust stability of the whole closed-loop system.

Key words: guardian maps, hypersonic vehicles, adaptive control, linear parameter varying (LPV), wide flight envelope control

中图分类号:

V249.1

肖地波, 陆宇平, 刘燕斌, 许晨. 应用保护映射理论的高超声速飞行器自适应控制律设计[J]. 航空学报, 2015, 36(10): 3327-3337.

XIAO Dibo, LU Yuping, LIU Yanbin, XU Chen. Adaptive control law design using guardian maps theory for hypersonic vehicles[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(10): 3327-3337.

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

应用保护映射理论的高超声速飞行器自适应控制律设计

Adaptive control law design using guardian maps theory for hypersonic vehicles

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