[1] 芮筱亭,陆毓琪,王国平,等. 多管火箭发射动力学仿真与试验测试方法[M].北京:国防工业出版社,2003. RUI Xiao-ting, LU Yu-qi, WANG Guo-ping, et al. Simulation and test methods of launch dynamics of multiple launch rocket system[M]. Beijing: National Defense Industry Press,2003. (in Chinese) [2] 展志焕,芮筱亭,戎保,等. 多管火箭定向管振动控制设计[J]. 振动工程学报, 2011, 24(3): 603-607. ZHAN Zhi-huan, RUI Xiao-ting, RONG Bao, et al. Design of vibration control of launcher for multiple launch rocket system[J].Journal of Vibration Engineering, 2011, 24(3): 603-607 (in Chinese) [3] 芮筱亭,王国平,贠来峰,等. 某远程多管火箭振动特性研究[J]. 振动与冲击, 2005, 24(1): 9-12. RUI Xiao-ting, WANG Guo-ping, YUN Lai-feng, et al. Study on the vibration characteristics of LRMLRS[J]. Journal of Vibration and Shock, 2005, 24(1): 9-12. (in Chinese) [4] 徐伟国,毕世华,陈阵.发射装置支撑刚度对火箭弹初始扰动的影响研究[J]. 兵工学报, 2008, 29(6):709-712. XU Wei-guo, BI Shi-hua, CHEN Zhen. Study on the influence of the launcher support stiffness on rocket initial disturbances[J]. Acta Armamentarii, 2008, 29(6): 709-712. (in Chinese) [5] 王国平,芮筱亭,陆毓琪.射序对多管火箭武器性能影响分析[J].南京理工大学学报,2004, 28(4):364-368. WANG Guo-ping, RUI Xiao-ting, LU Yu-qi. Influence of firing orders on performance of MLRS[J]. Journal of Nanjing University of Science and Technology, 2004, 28(4):364-368. (in Chinese) [6] 芮筱亭,贠来峰,陆毓琪,等.多体系统传递矩阵法及其应用[M].北京:科学出版社,2008. RUI Xiao-ting, YUN Lai-feng, LU Yu-qi, et al. Transfer matrix method of multibody system and its applications [M]. Beijing: Science Press, 2008. (in Chinese) [7] Rui X T, Wang G P, Lu Y Q. et al. Transfer matrix method for linear multibody system[J]. Multibody System Dynamics, 2008, 19(3): 179-207. [8] Rui X T, Rong B, Wang G P, et al. Discrete time transfer matrix method for dynamics analysis of complex weapon systems[J]. Science China Technological Sciences, 2011, 54(5): 1061-1071. |