Launch Dynamics Modeling and Simulation of Vehicular Missile System

Author:

Wang Xun1,Rui Xiaoting1,Yang Fufeng1,Zhou Qinbo1

Affiliation:

1. Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China

Funder

Natural Science Foundation of China Government

Research Found for the Doctoral Program of Higher Education of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference16 articles.

1. RuiX. T., Launch Dynamics of Multibody Systems, National Defense Industry Press, Beijing, 1995, pp. 1–7 (in Chinese).

2. YaoC. R.TangG. L.SongT. L., Launch Dynamics of Rocket and Missile, Beijing Institute of Technology Press, Beijing, 1996, pp. 5–16 (in Chinese).

3. Coupled-interaction launch behavior of a flexible rocket and flexible launcher

4. Research on the Initial Disturbance of Vehicular Missile with System Vibration Analysis

5. Modeling and verification of a missile launcher system

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