吸气式高超声速飞行器控制研究进展  

Review of control on air-breathing hypersonic flight vehicle

作　　者：王鹏飞 刘红琴 杨自牧 杨维熙 Wang Pengfei;Liu Hongqin;Yang Zimu;Yang Weixi(Army Academy of Artillery and Air Defence,Hefei 230031,China;95037 Army,Wuhan 430000,China)

机构地区：[1]陆军炮兵防空兵学院,合肥230031 [2]95037部队,武汉430000

出　　处：《空天技术》2024年第5期33-43,共11页Aerospace Technology

基　　金：安徽省自然科学基金(2008085QF332);学院自主科研项目(PPXY220101014)。

摘　　要：针对吸气式高超声速飞行器(Air-Breathing Hypersonic Flight Vehicle,AHFV)的动力学特征,对其控制研究现状进行了综述。从控制的角度归纳了AHFV具备的强烈耦合性、显著非线性、高度不确定性、快速时变性以及非最小相位特性等复杂动力学特征,分析了这些特征给控制器设计带来的挑战;结合线性变参数控制、有限时间控制、事件触发控制、预设性能控制和浸入与不变控制等几种较为新颖的控制理论,探讨了AHFV控制方法的研究现状;从工程实用的角度出发,对AHFV控制系统的热点问题进行了梳理;最后的研究结论可为后续该领域研究提供思路借鉴。According to the dynamic characteristics of air-breathing hypersonic flight vehicle(AHFV),a review of the current research on the control of is conducted.From a control perspective,the complex dynamic characteristics of AHFV are summarized,such as strong coupling,significant nonlinearity,high uncertainty,rapid time-varying behavior,and non-minimum phase properties,and then the challenges these characteristics pose to controller design are analyzed.By combining several common nonlinear control theories including linear parameter varying control,finite-time control,event-triggered control,prescribed performance control and immersion&invariance control,the current research status of AHFV control system design is given.Starting from an engineering practical perspective,the hot issues in AHFV control systems are discussed.Finally,the insights for future research in this field are offered by conclusion.

关 键 词：吸气式高超声速飞行器 动力学特征 非线性控制理论 事件触发控制 浸入与不变控制 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]