BOLLINO K P.High-fidelity real-time trajectory optimization for reusable launch vehicles[D].Monterey,California,USA:Naval Ostgraduate School,2006.
[2]
LU Ping,XUE Song-bai.Rapid generation of accurate entry landing footprints[C]//AIAA Guidance,Navigation and Control Conference.Chicago,Illinois:AIAA,2009.
[3]
赵汉元.飞行器再入动力学和制导[M].长沙:国防科技大学出版社,1997.
[4]
ZHAO Han-yuan.Dynamics and guidance of a reentry vehicle[M].Changsha:National University of Defense Technology Press,1997.(in Chinese)
[5]
HUNTINGTON G T.Advancement and analysis of a Gauss pseudospectral transcription for optimal control problems[D].Massachusetts,USA:Massachusetts Institute of Technology,2007:51-57,115-143.
[6]
RAO A V,BENSON D A,DARBY C L.Algorithm:GPOPS,a Matlab software for solving multiple-phase optimal control problems using the Gauss pseudospectral method[J].ACM Transactions on Mathematical Software,2010,37(2):1-39.
YAN Xiao-dong,TANG Shuo.Entry trajectory tracking law for suborbital launch vehicle via feedback linearization[J].Journal of Astronautics,2008,29(5):1 546-1 550(in Chinese)