JAROSLAW S S.Sensitivity analysis and multidisciplinary optimization for aircraft design:recent advances and results[J].Journal of Aircraft,1990,27(12):993-1001.
[2]
BROWN N F,OLDS J R.Evaluation of multidisciplinary optimization techniques applied to a reusable launch vehicle[J].Journal of Spacecraft and Rockets,2006,43(6):1 289-1 300.
[3]
BRAUN R D,POWELL R W.Comparison of two multidisciplinary optimization strategies for launch-vehicle design[J].Journal of Spacecraft and Rockets,1995,32(3):404-410.
YANG Jun,CHEN Ru-xun,ZHAO Xi-liang.Integral optimization design for tactical rocket and it’s SRM by utilizing the synthesis of internal ballistics and trajectory[J].Journal of Astronautics,1999,20(1):21-27.(in Chinese)
[6]
龙乐豪.总体设计[M].北京:中国宇航出版社,1989.
[7]
LONG Le-hao.Overall design[M].Beijing:China Astronautic Publishing House,1989.(in Chinese)
[8]
贾沛然,陈克俊,何力.远程火箭弹道学[M].长沙:国防科技大学出版社,1994.
[9]
JIA Pei-ran,CHEN Ke-jun,HE Li.The ballistics of long-range rocket[M].Changsha:National University of Defense Technology Press,1994.(in Chinese)
PRICE K.Differential evolution vs.the functions of the 2nd ICEO[C]//IEEE Int Conf on Evolutionary Computation.Indian Upolis:IEEE,1997:153-157.
[12]
HONG Bei,LIANG Xin-xin,XIN Wan-qing.Multi-constraint trajectory optimization for solid launch vehicle[J].Missiles and Space Vehicles,2012,(3):1-5.(in Chinese)
[13]
PRICE K.Differential evolution:a fast and simple numerical optimizer[C]//Biennial Conf of the North American Fuzzy Information Processing Sociey.New York:IEEE 1996:524-527.