无模型自适应控制在飞行控制系统中的应用综述  

Review on application of model-free adaptive control in flight control systems

作　　者：温奇峰 张骄阳 樊慧津[1,2] 刘磊[1,2] 王博[1,2] Wen Qifeng;Zhang Jiaoyang;Fan Huijin;Liu Lei;Wang Bo(School of Artificial Intelligence and Automation,Huazhong University of Science and Technology,Wuhan 430074,China;National Key Laboratory of Science and Technology on Multispectral Information Processing,Huazhong University of Science and Technology,Wuhan 430074,China)

机构地区：[1]华中科技大学人工智能与自动化学院,武汉430074 [2]华中科技大学多谱信息处理国家级重点实验室,武汉430074

出　　处：《战术导弹技术》2024年第4期41-52,91,共13页Tactical Missile Technology

基　　金：武汉市知识创新专项项目基础研究(2023010201010055)。

摘　　要：飞行控制系统普遍存在难以精确建模的问题,而无模型自适应控制作为一种典型的数据驱动的控制方法,其控制律的更新仅依赖于系统的输出数据,在飞行控制系统中显示出广泛的应用前景。本文综述了无模型自适应控制在飞行控制系统中的近期发展。总结了该控制方法在处理飞行控制系统面对的不同挑战时给出的解决方案。针对用于执行在轨服务的航天器,即组合体飞行器,分析了无模型自适应控制方法的优越性,介绍了其应用和发展现状。对无模型自适应控制方法在飞行控制系统中的进一步应用与发展进行了展望。Generally,flight control systems face the issue of being hard to precisely model,Whereas,as a typical data-driven control method,model-free adaptive control(MFAC)only relies on the system output data to update its control law,thereby showing a wide application prospect in flight control systems.The recent development of MFAC in flight control systems is reviewed.the solutions to different challenges in flight control systems offered by this control method is summarized.For the combined aircrafts of performing onorbit service,the superiority of the MFAC method is analyzed,and their applications and current development status are presented.The further application and development of MFAC method in flight control system is prospected.

关 键 词：无模型自适应控制 数据驱动 姿态控制 飞行控制系统 变外形飞行器 组合体飞行器 

分 类 号：TP11[自动化与计算机技术—控制理论与控制工程]