李惠峰,谢陵.基于预测校正方法的RLV再入制导律设计[J].北京航空航天大学学报,2009,35(11):1344-1348 Li Huifeng,Xie Ling.Reentry guidance law design for RLV based on predictor-corrector method[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(11):1344-1348(in Chinese)
[2]
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,1997:382-411 Zhao Hanyuan.Fight vehicle reentry dynamics and guidance[M].Changsha:National University of Defense Technology Press,1997:382-411(in Chinese)
[3]
Xue Songbai,Lu Ping.Constrained predictor-corrector entry guidance[J].Journal of Guidance,Control,and Dynamics,2010,33(4):1273-1281
[4]
Mease K D,Chen D T,Teufel P,et al.Reduced-order entry trajectory planning for acceleration guidance[J].Journal of Guidance,Control and Dynamics,2002,25(2):257-266
[5]
Kumar R,Ganguli R,Omkar S N,et al.Rotorcraft parameter identification from real time flight data[J].Jounal of Aircraft,2008,45(1):333-341
[6]
Morelli E A,Derry S D,Smith M S.Aerodynamic parameter estimation for the X-43A (Hyper-X) from flight data .AIAA 2005-5921,2005
[7]
Kumar R,Ganguli R,Omkar S N,et al.Rotorcraft parameter identification from real time flight data[J].Jounal of Aircraft,2008,45(1):333-341
[8]
Xue Songbai,Lu Ping.Constrained predictor-corrector entry guidance[J].Journal of Guidance,Control,and Dynamics,2010,33(4):1273-1281
[9]
Hu Jianxue,Chen Kejun,Zhao Hanyuan,et al.Hybrid entry guidance for reusable launch vehicles [J].Journal of Astronautics,2007,28(1):213-217
[10]
余舜京,程燕青,钱炜祺.跨声速气动参数在线辨识方法[J].宇航学报,2011,32(6):1211-1216 Yu Shunjing,Cheng Yanging,Qian Weiqi.Research on transonic aerodynamic parameter online identification[J].Journal of Astronautics,2011,32(6):1211-1216(in Chinese)
[11]
Morelli E A,Derry S D,Smith M S.Aerodynamic parameter estimation for the X-43A (Hyper-X) from flight data .AIAA 2005-5921,2005
[12]
Hu Jianxue,Chen Kejun,Zhao Hanyuan,et al.Hybrid entry guidance for reusable launch vehicles [J].Journal of Astronautics,2007,28(1):213-217
[13]
李惠峰,谢陵.基于预测校正方法的RLV再入制导律设计[J].北京航空航天大学学报,2009,35(11):1344-1348 Li Huifeng,Xie Ling.Reentry guidance law design for RLV based on predictor-corrector method[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(11):1344-1348(in Chinese)
[14]
余舜京,程燕青,钱炜祺.跨声速气动参数在线辨识方法[J].宇航学报,2011,32(6):1211-1216 Yu Shunjing,Cheng Yanging,Qian Weiqi.Research on transonic aerodynamic parameter online identification[J].Journal of Astronautics,2011,32(6):1211-1216(in Chinese)