Application of constraint force equation method for missile launching dynamics modeling

[1] 姚昌仁,唐国梁,宋廷伦．火箭导弹发射动力学[M]．北京:北京理工大学出版社,1996:6-7 Yao Changren,Tang Guoliang,Song Tinglun．Launching dynamics for rockets or missiles[M]．Beijing:Beijing Institute of Technology Press,1996:6-7(in Chinese) [2] Toniolo M D,Tartabini P V,Pamadi B N,et al．Constraint force equation methodology for modeling multi-body stage separation dynamics[R]．AIAA-2008-219,2008 [3] Tartabini P V,Roithmayr C,Toniolo M D,et al．Verification of the constraint force equation methodology for modeling multibody stage separation[R]．AIAA-2008-7039,2008 [4] 薛明旭．战术导弹发射动力学与仿真[D]．西安:西北工业大学航天学院,2004 Xue Mingxu．Launch dynamics of tactical missile and simulation[D]．Xi’an:College of Astronautics,Northwestern Polytechnical University,2004(in Chinese) [5] 周慧钟,李忠应,王瑾玫．有翼导弹飞行动力学[M]．北京:航空专业教材编审组,1983:11-19 Zhou Huizhong,Li Zhongying,Wang Jinmei．Winged missile flight dynamics[M]．Beijing: Aeronautics Professional Teaching Material Edit Group,1983:11-19(in Chinese) [6] 邵伟龙,陈万春．吸气式导弹分离动力学建模与仿真分析[C]／／2006年中国飞行力学年会论文集.黄山市:中国宇航学会空气动力学与飞行力学专业委员会,2006:221-225 Shao Weilong,Chen Wanchun．Modeling,simulation and analysis of the air-breathing missile separation dynamics[C]//2006 China Flight Dynamics Annual Conferences.HuangShan:Chinese Society of Astronautics Aerodynamics and Flight Dynamics Committee,2006:221-225(in Chinese) [7] 肖业伦,陈万春．飞行器相对姿态运动的静力学、运动学和动力学方法[J]．中国空间科学技术,2003,10(5):10-15 Xiao Yelun,Chen Wanchun．Statical,kinematical and dynamical approaches for treating the relative attitude motion of flight vehicles[J]．Chinese Space Science and Technology,2003,10(5):10-15(in Chinese)