Atkins E.Dynamic waypoint generation given reduced flight performance .AIAA-2004-779,2004
[2]
Strube M J.Post-failure trajectory planning from feasible trim state sequences .College Park:Dept of Aerospace Engineering,University ofMaryland at College Park,2005
[3]
Oppenheimer M W,Doman D B,Bolender M A.A method for estimating control failure effects for aerodynamic vehicle trajectory retargeting .AIAA-2004-5169,2004
[4]
Fahroo F,Doman D.A direct method for approach and landing trajectory reshaping with failure effect estimation .AIAA-2004-4772,2004
[5]
Betts J T.Survey of numerical methods for trajectory optimization[J].Journal of Guidance,Control and Dynamics,1998,21(2):193-206
[6]
雍恩米,陈磊,唐国金.飞行器轨迹优化数值方法综述[J].宇航学报,2008,29(2):397-406 Yong Enmi,Chen Lei,Tang Guojin.A survey of numerical methods for trajectory optimization of spacecraft[J].Journal of Astronautics,2008,29(2):397-406(in Chinese)
[7]
肖业伦.航空航天器运动的建模[M].北京:北京航空航天大学出版社,2003:18-37 Xiao Yelun.Modeling of aircraft and spacecraft motion[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2003:18-37(in Chinese)
[8]
Yakimenko O A,Xu Y,Basset G.Computing short-time aircraft maneuvers using direct methods .AIAA-2008-6632,2008
[9]
Morelli E A.Global nonlinear aerodynamic modeling using multivariate orthogonal functions[J].Journal of Aircraft,1995,32(2):270-277
[10]
Benson D A,Huntington G T,Thorvaldsen T P,et al.Direct trajectory optimization and costate estimation via an orthogonal collocation method .AIAA-2006-6358,2006