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针对吸气式高超声速飞行器的控制系统设计问题,对其研究现状进行了梳理。从分析吸气式高超声速飞行器的独特动力学特征入手,总结吸气式高超声速飞行器控制系统设计的特点和难点。基于主流的建模方法和飞行控制理论,从动力学建模和控制器构造两个方面对吸气式高超声速飞行器控制系统的研究现状进行了分析。对当前吸气式高超声速飞行器控制系统研究存在的主要问题进行了总结,为后续的控制系统设计明确了改进方向。
Abstract：The research progresses on control system design for air-breathing hypersonic flight vehicle( AHV) are reviewed. Firstly,the features and difficulties of controller designing are summarized base on the particular dynamic characteristics of AHV. Then,the developments of dynamic modeling and controller designing for AHV are elaborated with typical modeling approach and flight control strategies. Finally,the defects of the existing research on flight control of AHV are pointed,which indicates some feasible research orientations in the control system design for AHV.
[1]黄志澄.高超声速飞行器空气动力学[M].北京:国防工业出版社,1995.
[2]Shaughnessy J,Pinckney S,McMinn J,et al.Hypersonic vehicle simulation model:Winged-cone configuration[R].NASA-102610,NASA,1990.
[3]Schmidt D.Dynamics and control of hypersonic aeropropulsive/aeroelastic vehicles[R].AIAA-92-4326-CP,AIAA,1992.
[4]Chavez F,Schmidt D.Analytical aeropulsive/aeroelastic hypersonic-vehicle model with dynamic analysis[J].Journal of Guidance Control and Dynamics,1994,17(6):1308-1319.
[5]Bilimoria K,Schmidt D.Integrated development of the equations of motion for elastic hypersonic flight vehicles[J].Journal of Guidance Control and Dynamics,1995,18(1):50-65.
[6]Mirmirani M,Wu C,Clark A,et al.Modeling for control of a generic air-breathing hypersonic vehicle[C].Proceedings of Guidance,Navigation,and Control Conference and Exhibit.San Francisco,California:AIAA,2005:3959-3977.
[7]Keshmiri S,Mirmirani M D,Colgren R D.Six-DOFmodeling and simulation of a generic hypersonic vehicle for conceptual design studies[C].Proceedings of Modeling and Simulation Technologies Conference.Providence,Rhode Island:AIAA,2004:1-12.
[8]Bolender M A,Doman D B.Nonlinear longitudinal dynamical model of an air-breathing hypersonic vehicle[J].Journal of Spacecraft and Rockets,2007,44(2):374-387.
[9]Parker J T,Serrania A,Yurkovich S,et al.Control-oriented modeling of an air-breathing hypersonic vehicl[J].Journal of Guidance,Control,and Dynamics,2007,30(3):856-869.
[10]吴宏鑫,胡军,谢永春.基于特征模型的智能自适应控制[M].北京:中国科学技术出版社,2009.
[11]孟斌,吴宏鑫.一类飞行器姿态动力学特征建模研究[J].中国科学:技术科学,2010,40(8):898-902.
[12]王明昊,刘刚,赵鹏涛,等.高超声速飞行器的LPV变增益状态反馈H∞控制[J].宇航学报,2013,34(4):488-496.
[13]后德龙,王青,董朝阳,等.高超声速飞行器切换多胞系统自适应跟踪控制[J].系统工程与电子技术,2014,36(5):926-932.
[14]刘晓韵,王静,李宇明.基于反馈线性化/LQR方法的高超声速飞行器姿控系统设计[J].航天控制,2014,32(4):37-41.
[15]杜立夫,黄万伟,刘晓东,等.考虑特征模型的高超声速飞行器全通道自适应控制[J].宇航学报,2016,37(6):711-720.
[16]高海燕,蔡远利.高超声速飞行器的滑模预测控制方法[J].西安交通大学学报,2014,48(1):68-72.
[17]Tian B L,Su R,Fan W R.Multiple-time scale smooth second order sliding mode controller design for flexible hypersonic vehicles[J].Journal of Aerospace Engineering,2015,229(5):781-791.
[18]Wang P F,Wang J,Shi J M,et al.Adaptive neural back-stepping control with constrains for a flexible airbreathing hypersonic vehicle[J].Mathematical Problems in Engineering,2015,(11):1-14.
[19]Wang P F,Wang J,Bu X W,et al.Adaptive fuzzy back-stepping control of a flexible air-breathing hypersonic vehicle subject to input constraints[J].Journal of Intelligent&Robotic Systems,2016,(11):1-18.
[20]Xu B,Wang S X,Gao D X,et al.Command filter based robust nonlinear control of hypersonic aircraft with magnitude constraints on states and actuators[J].Journal of Intelligent and Robotic Systems,2014,73:233-247.
[21]Ji Y H,Zong Q and Zhou H L.Command filtered backstepping control of a flexible air-breathing hypersonic flight vehicle[J].Journal of Aerospace Engineering,2014,228(9):1617-1626.
[22]王鹏飞,王洁,罗畅,等.高超声速飞行器输入受限反演鲁棒控制[J].控制与决策,2017,32(2):232-238.
[23]Wang Y F,Jiang C S,Wu Q X.Attitude tracking control for variable structure near space vehicles based on switched nonlinear systems[J].Chinese Journal of Aeronautics,2013,26(1):186-192.
[24]Xu B,Yang C G,Pan Y P.Global neural dynamic surface tracking control of strict-feedback systems with application to hypersonic flight vehicle[J].IEEE Transactions on Neural Networks and Learning Systems,2015,26(10):2563-2575.
[25]Buschek H,Calise A.Fixed order robust control design for hypersonic vehicles[C].Proceedings of Guidance,Navigation and Control Conference.Washington,DC:AIAA,1994:3662-3694.
[26]Wu G,Meng X.Nonlinear disturbance observer based robust backstepping control for a flexible air-breathing hypersonic vehicle[J].Aerospace Science and Technology,2016,54:174-182.
[27]Hu Q,Meng Y.Adaptive backstepping control for airbreathing hypersonic vehicle with actuator dynamics[J].Aerospace Science and Technology,2017,67:412-421.
[28]Yang J,Zhao Z H,Li S H,et al.Composite predictive flight control for air-breathing hypersonic vehicles[J].International Journal of Control,2014,87(9):1970-1984.
Basic Information:
DOI：10.16358/j.issn.1009-1300.2019.9.008
China Classification Code:V249.1
Citation Information:
[1]王鹏飞,王光明,吴豫杰,等.吸气式高超声速飞行器控制技术研究综述[J].战术导弹技术,2019,No.195(03):12-18.DOI:10.16358/j.issn.1009-1300.2019.9.008.
Fund Information:
国家自然科学基金(61603410)