[1] LIU X D, ZHANG Y, WANG S, et al. Backstepping attitude control for hypersonic gliding vehicle based on a robust dynamic inversion approach[J].Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2014, 228(8):543-552.
[3] YOUNG M, KEITH S, PANCOTTI A. An overview of advanced concepts for near-space systems[R].AIAA-2009-4805, 2009.doi:10.2514/6.2009-4805.
[8] XU H, MIRMIRANI M D, IOANNOU P A. Adaptive sliding mode control design for a hypersonic flight vehicle[J].Journal of Guidance, Control, and Dynamics, 2004, 27(5):829-838.
[9] SUN H, LI S, SUN C. Finite time integral sliding mode control of hypersonic vehicles[J].Nonlinear Dynamics, 2013, 73(1/2):229-244.
[10] SHTESSEL Y, MCDUFFIE J, JACKSON M, et al.Sliding mode control of the X-33 vehicle in launch and re-entry modes[C]//AIAA Guidance, Navigation and Control Conference, 1998:1352-1362.
[11] YU S, YU X, SHIRINZADEH B, et al.Continuous finitetime control for robotic manipulators with terminal sliding mode[J].Automatica, 2005, 41(11):1957-1964.
[12] MEI H, WANG Y. Fast convergent sliding mode variable structure control of robot[J].Information and Control, 2009, 38(5):552-557.
[17] KESHMIRI S, COLGREN R, MIRMIRANI M. Six-DOF modeling and simulation of a generic hypersonic vehicle for control and navigation purposes[C]//AIAA Gui-dance, Navigation and Control Conference, 2006.doi:10.2514/6.2006-6694.
[20] MORIMOTO H.Trajectory optimization for a hypersonic vehicle with constraint[D].Atlanta: Georgia Institute of Technology, 1997.