[1] RODRIGUEZ A A,DICKESON J J,CIFDALOZ O,et al. Modeling and control of scramjet-powered hypersonic vehicles:Challenges,trends,& tradeoffs:AIAA-2008-6793[R].Reston:AIAA,2008.
[2] LAMORTE N,FRIEDMANN P P,DALLE D J,et al.Uncertainty propagation in integrated airframe-propulsion system analysis for hypersonic vehicle[J].Journal of Propulsion and Power,2015,31(1):54-68.
[3] DICKESON J J,RODRIGUEZ A A,SRIDHARAN S,et al.Control-relevant modeling,analysis,and design for scramjet-powered hypersonic vehicle:AIAA-2009-7287[R].Reston:AIAA,2009.
[4] KARLGARD C D,MARTIN J G,TARTABINI P V,et al.Hyper-X Mach 10 trajectory reconstruction:AIAA-2005-5920[R].Reston:AIAA,2005.
[5] MORELLI E A.Flight test experiment design for characterizing stability and control of hypersonic vehicles[J].Journal of Guidance,Control,and Dynamics,2009,32(3):949-959.
[6] 孙长银,穆朝絮,余瑶.近空间高超声速飞行器控制的几个科学问题研究[J].自动化学报,2013,39(11):1901-1913.SUN C Y,MU Z X,YU Y.Some control problem for near space hypersonic vehicles[J].Acta Automatica Sinica,2013,39(11):1901-1913(in Chinese).
[7] WANG Q,STENGEL R F.Robust nonlinear control of a hypersonic aircraft[J].Journal of Guidance,Control,and Dynamics,2000,23(4):577-585.
[8] FIORENTINI L,SERRANI A,BOLENDER M A,et al.Nonlinear robust adaptive control of flexible air-breathing hypersonic vehicles[J].Journal of Guidance,Control,and Dynamics,2009,32(2):401-416.
[9] SUN H B,LI S H,SUN C Y.Finite time integral sliding model control of hypersonic vehicles[J].Nonlinear Dynamics,2013,73(1/2):229-244.
[10] 刘燕斌,陆宇平.基于反步法的高超音速飞机纵向逆飞行控制[J].控制与决策,2007,22(3):313-317.LIU Y B,LU Y P.Longitudinal inversion flight control based on backstepping for hypersonic vehicle[J].Control and Decision,2007,22(3):313-317(in Chinese).
[11] 黄喜元,王青,董朝阳.基于Backstepping的高超声速飞行器鲁棒自适应控制[J].系统工程与电子技术,2011,33(6):1321-1326.HUANG X Y,WANG Q,DONG C Y.Robust adaptive control of hypersonic vehicles via Backstepping method[J].Systems Engineering and Electronics,2011,33(6):1321-1326(in Chinese).
[12] XU B,GAO D X,WANG S X.Adaptive neural control based on HGO for hypersonic flight vehicles[J].Science China Information Sciences,2011,54(3):511-520.
[13] XU B,FAN Y H,ZHANG S M.Minimal-learning-parameter technique based adaptive neural control of hypersonic flight dynamics without back-stepping[J].Neurocomputing,2015,164(C):201-209.
[14] SWAROOP D,HEDRICK J K,YIP P P,et al.Dynamic surface control for a class of nonlinear systems[J].IEEE Transactions on Automatic Control,2000,45(10):1893-1899.
[15] XU B,HUANG X Y,WANG D W,et al.Dynamic surface control of constrained hypersonic flight models with parameter estimation and actuator compensation[J].Asian Journal of Control,2014,16(1):162-174.
[16] WASEEM A B,LIN Y,KENDRICK A S.Adaptive integral dynamic surface control of a hypersonic flight vehicle[J].International Journal of Systems Science,2015,46(10):1717-1728.
[17] 韩京清,王伟.非线性跟踪微分器[J].系统科学与数学,1994,14(2):177-183.HAN J Q,WANG W.Nonlinear tracking-differentiator[J].Journal of Systems Science and Mathematical Science,1994,14(2):177-183(in Chinese).
[18] PARKER J T,SERRANI A,YURKOVICH S,et al.Control-oriented modeling of an air-breathing hypersonic vehicle[J].Journal of Guidance,Control,and Dynamics,2007,30(3):856-869.
[19] XU B,SHI Z K.An overview on flight dynamic and control approaches for hypersonic vehicles[J].Science China Information Sciences,2015,58(7):1-19.
[20] FIORENTINI L,SERRANI A.Adaptive restricted trajectory tracking for a non-minimum phase hypersonic vehicle model[J].Automatic,2012,48(7):1248-1261.
[21] GUO B Z,ZHAO Z L.On convergence of tracking differentiator[J].International Journal of Control,2001,84(4):693-701. |