[1] 徐延万. 控制系统[M]. 北京: 中国宇航出版社, 1989. Xu Yanwan. Control system[M]. Beijing: China Astronautic Publishing House, 1989. (in Chinese)
[2] 朱忠惠. 推力矢量控制伺服系统[M]. 北京: 中国宇航出版社, 1995. Zhu Zhonghui. Servo system of thrust vector control[M]. Beijing: China Astronautic Pubishing House, 1995. (in Chinese)
[3] 赵迎鑫, 张晓莎, 赵守军, 等. 新型大推力发动机负载动态模型的获取和识别方法[J]. 流体传动与控制, 2008(5): 41-43. Zhao Yingxin, Zhang Xiaosha, Zhao Shoujun, et al. A method for obtaining and identifying dynamic model of a new engine with large thrust[J]. Fluid Power Transmission and Control, 2008(5): 41-43.(in Chinese)
[4] Soccodato C, Ruault J M. Ariane 5 launch vehicle—from concepts to future evolutions. AIAA-1999-2906, 1999.
[5] Sowers G. First flight—Atlas V evolved expendable launch vehicle. AIAA-2002-4204, 2002.
[6] Slazer F A, Harvey J C, Sirko R J, et al. Delta IV launch vehicle growth options to support NASA’s space exploration vision[J]. Acta Astronautica, 2005, 57(2-8): 604-613.
[7] Lillie C F,Dailey D, Polidan R S. Large aperture telescopes for launch with the Ares V launch vehicle[J]. Acta Astronautica, 2010, 66(3-4):374-381.
[8] K. C. 柯列斯尼可夫, B. H. 苏霍夫. 作为自动控制对象的弹性飞行器[M]. 关世义, 常伯浚, 译. 北京: 国防工业出版社, 1979. К.С. КОЛЕСНИКОВ, В.Н. СУХОВ. Flexible aerocraft as object of automatic control system[M]. Guan Shiyi, Chang Bojun, translated. Beijing: National Defense Industry Press, 1979. (in Chinese)
[9] Greensite A L. Analysis and design of space vehicle flight control system[M]. New York: Spartan Books, 1970.
[10] Dhekane M V, Lalithambika V R, Dasgupta D S, et al. Modeling of control/structure interaction in launch vehicle—a flight experience[J]. AIAA-1999-4132, 1999.
[11] Oheroi S, Janardhanan S, Bandyopadhyay B. Output feedback control of practical launch vehicle systems//Proceedings of the 2004 IEEE Intemational Conference on Control Applications. 2004.
[12] Graham R E, Center L R, Cleveland O. Effect of gimbal friction modeling technique on control stability and performance for centaur upper-stage. NASA-TM-89894, 1987.
[13] Dhabale A, Banavar R N, Dhekane M V. LQG controller designs from reduced order models for a launch vehicle[J]. Sadhana, 2008, 33(1): 1-14.
[14] 郑大钟. 线性系统理论[M]. 北京: 清华大学出版社, 2002. Zheng Dazhong. Linear system theory[M]. Beijing: Tsinghua University Press, 2002. (in Chinese) |