Automatic Deduction Method of the Overall Transfer Equation of a New Type Multiple Launch Rocket Systems

摘要：

　　The automatic deduction method to overall transfer equation and rapid simulation of launch dynamics of Multiple Launch Rocket Systems(MLRS)are the key to the dynamic design of MLRS.In order to further improve the modeling efficiency and the programming level,an automatic method to develop the overall transfer equations for a new type MLRS is developed.As a new dynamics method of multibody systems,the Transfer Matrix Method for Multibody System(MSTMM)can be widely used in the dynamics analysis and design of various mechanical systems,such as multiple launch rocket systems,self-propelled artilleries and naval guns for its features as follows: without global dynamics equations of the system; high programming; low order of matrix involved and high computational speed.The programming level of the study on the dynamics of the new type MLRS has been improved by using this method.The launch dynamics are simulated rapidly by proposed method.The theory base for visual simulation system and dynamic design for dynamics of MLRS is provided.

关键词： New Type Multiple Launch Rocket System Transfer Matrix Method for Multibody System Overall Transfer Equations Overall Transfer Matrix Automatic

作者: Song XIN Xiaoting RUI Jianshu ZHANG Guoping WANG Zhe ZHOU

作者单位: Institute of launch dynamics,Nanjing University of Science & Technology,Nanjing 210094,P.R.China

会议类型: 国际会议

会议名称: The 5th International Conference on Mechanical Engineering and Mechanics(第五届国际机械工程与力学会议)

会议地点: 江苏扬州

会议语种:英文

页码: 75-81

在线出版日期: 2014-08-21（万方平台首次上网日期，不代表论文的发表时间）