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Dynamics Control of Rocket Launching Systems(PDF)

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2002年02期
Page:
139-143
Research Field:
Publishing date:
2002-04-30

Info

Title:
Dynamics Control of Rocket Launching Systems
Author(s):
ZhangDingguo ZhangFuxiang ①
School of Sciences,① School of Mechanical Engineering,NUST,Nanjing 210094
Keywords:
rocket launching systems dynamics cont rol driver const raint method
PACS:
TJ393
DOI:
-
Abstract:
This paper discusses the problem of dynamics cont rol for rocket launching systems. The t radit ional method for dynamics cont rol, Driver Constraint Method, is int roduced, and it s cont rolling thoughts are narrated in detail. A set of governing dif ferent ial equat ions for mult-i body model of rocket gun systems is established via employ ing the Driver Constraint Method. Based on these equat ions, a softw are is developed. And an example, the dy namics cont rol of a rocket gun system, is given to demonst rate the cont rol procedure and the control effect. Suitable dynamics cont rol exerted on a rocket launching system is beneficial to the suppression of the v-i brat ion and the reduct ion of the init ial disturbance of rocket .

References:

1 Cochran J E. Launcher as passive controllers. AD- 096801, 1980
2 Cochran J E. Launcher/ rocket syst em dynamics and passive cont rol. AIAA- 81- 190 2, 1981
3 Cochran J E, Richard J. Rocket launchers as passive controllers ( final report) . AD- A112 571,1981
4 刘延柱, 洪嘉振, 杨海兴1 多刚体系统动力学1 北京: 高等教育出版社, 1989
5 章定国1 火箭发射系统动力学仿真与控制研究: [ 博士学位论文] 1 南京: 南京理工大学, 1998

Memo

Memo:
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Last Update: 2002-04-30