Proceedings of the 6th International Conference on Electronic, Mechanical, Information and Management Society

Study on the Vibration Characteristics of a complex Multiple launch rocket system

Authors
Wenbing Tang, Xiaoting Rui, Fufeng Yang, Feifei Liu
Corresponding Author
Wenbing Tang
Available Online April 2016.
DOI
https://doi.org/10.2991/emim-16.2016.79How to use a DOI?
Keywords
Vibration characteristics; Transfer matrix method for multibody system; Multiple launch rocket system; Modal test.
Abstract
Transfer matrix method for multibody system (MSTMM) is a new and efficient method for multibody system dynamics (MSD) developed in recent 20 years. Based on many advantages of MSTMM in studying MSD, the rapid and accurate computation problem of vibration characteristics of a complex multiple launch rocket system (MLRS) are solved in this paper. The dynamics model, the transfer equations of elements, the overall transfer equation and the eigenfrequency equation are established. The results got by MSTMM were validated by modal tests, and compared with ordinary dynamics method, the computational speed has been increased 65 times.
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Proceedings
6th International Conference on Electronic, Mechanical, Information and Management Society
Part of series
Advances in Computer Science Research
Publication Date
April 2016
ISBN
978-94-6252-176-6
ISSN
2352-538X
DOI
https://doi.org/10.2991/emim-16.2016.79How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Wenbing Tang
AU  - Xiaoting Rui
AU  - Fufeng Yang
AU  - Feifei Liu
PY  - 2016/04
DA  - 2016/04
TI  - Study on the Vibration Characteristics of a complex Multiple launch rocket system
BT  - 6th International Conference on Electronic, Mechanical, Information and Management Society
PB  - Atlantis Press
SP  - 360
EP  - 365
SN  - 2352-538X
UR  - https://doi.org/10.2991/emim-16.2016.79
DO  - https://doi.org/10.2991/emim-16.2016.79
ID  - Tang2016/04
ER  -