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作 者:陈谋[1] 黄正国 申耀华 刘凡 CHEN Mou;HUANG Zhengguo;SHEN Yaohua;LIU Fan(College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China)
机构地区:[1]南京航空航天大学自动化学院,南京211106
出 处:《航空学报》2025年第6期27-58,共32页Acta Aeronautica et Astronautica Sinica
基 金:国家自然科学基金(U23B2036);江苏省科技计划专项资金港澳台科技合作项目(BZ2023057)。
摘 要:随着信息技术和人工智能技术的快速发展,先进飞行器在军事和民用领域的应用越来越广泛。但随着执行的任务和工作环境变得越来越复杂,使得对飞行控制的要求也越来越高。如何在外部干扰等综合影响下,保证先进飞行器飞行控制系统的鲁棒性与安全性是近年来的研究热点之一。基于国内外现有的研究成果,综述了先进飞行器复合抗干扰技术的研究现状并展望了未来的研究发展方向。主要从先进飞行器多种时变干扰下的多干扰观测器协同复合控制,时变干扰与未建模动态综合作用下的复合抗扰控制,输入/输出与状态约束下的复合抗扰控制,以及基于干扰耦合利用的复合抗扰控制几个方面,分析了相应复合抗干扰控制器设计原理,并综述了目前已解决的关键技术。最后,对先进飞行器复合抗干扰控制技术的未来研究方向进行了展望。With the rapid development of information technology and artificial intelligence technology,advanced vehicles have been applied more and more widely in military and civilian fields.However,with the increasing complexity of the mission itself and the mission environment,the requirements for flight control are also increasing.Therefore,how to ensure the robustness and safety of flight control systems under the comprehensive influence of external disturbance is one of the research hot spots in recent years.Based on the existing research results at home and abroad,this paper summarizes the research status of composite anti-disturbance technology for advanced vehicles and outlined its future research and development direction.The design principle of the corresponding composite antidisturbance control is analyzed mainly from the aspects of multi-disturbance observer composite control under multiple time-varying disturbances,composite anti-disturbance control under the combined action of time-varying disturbances and unmodeled dynamics,composite anti-disturbance control under input/output and state constraints,and composite anti-disturbance control based on disturbance coupling utilization.The key technologies that have been solved so far are reviewed.Finally,the future research directions of composite anti-disturbance control technology for advanced vehicles are discussed.
关 键 词:先进飞行器 复合抗干扰控制 干扰观测器 神经网络 输入约束 状态约束 输出约束
分 类 号:V24[航空宇航科学与技术—飞行器设计] TP273[自动化与计算机技术—检测技术与自动化装置]
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