[1] LANE S H,STENGEL R F.Flight control design using non-linear inverse dynamics[J].Automatica,1988,24(4): 471-483.
[2] VAN OORT E R,SONNEVELDT L,CHU Q P,et al.Full-envelope modular adaptive control of a flighter aircraft using orthogonal least aquares[J]. Journal of Guidance, Control,and Dynamics,2010,33(5):1461-1472.
[3] SHARMA M,RICHARDS N D.Adaptive integrated gui-dance and control for missile interceptors[R].AIAA-2004-4880,2004.
[4] PU M,WU Q X,JIANG C S,et al.New fast terminal sli-ding mode and its application to near space vehicles[J].Acta Aeronautica et Astronautica Sinica,2011,32(7):1283-1291.
[5] ZONG Q,WANG J,TIAN B L,et al.Quasi-continuous high-order sliding mode controller and observer design for flexible hypersonic vehicle[J].Aerospace Science and Technology,2013,27:127-137.
[6] ZHANG T Y,ZHOU J,GUO J G.Disign of predictive controller for hypersonic vehicles based on disturbance observer[J].Acta Aeronautica et Astronautica Sinica,2014, 35(1):215-222.
[7] KESHMINI S,COLGREN R,MIRMIRANI M.Six DOF nonlinear equations of motion for a generic hypersonic vehicle[R]. AIAA-2007-6626,Reston:AIAA,2007.