DocumentCode
2795792
Title
Dynamic simulation of rocket launch system based on virtual prototype technology
Author
Li, Peizhen
Author_Institution
Eng. Coll., Liyin Univ., Linyi, China
fYear
2011
fDate
15-17 July 2011
Firstpage
1258
Lastpage
1261
Abstract
The virtual prototype of multiply rocket launch system are built with dynamic simulation software-ADAMS. Constraining relations among rigid bodies are simulated Exterior force caused by multiply rocket launch system firing is analyzed Dynamic simulation is carried out when rocket firing. Curves of initial displacement of direction pipe and curves of initial velocity and acceleration of rocket projectile changing as time are obtained It can provide a theory foundation for evaluating dynamic characteristics of rocket launch system such as initial interference and improving its performance.
Keywords
aerospace computing; aerospace simulation; rockets; virtual prototyping; ADAMS; direction pipe; dynamic simulation; rocket launch system; rocket projectile; virtual prototype technology; Equations; Force; Mathematical model; Projectiles; Rockets; Solid modeling; Vibrations; dynamic simulation; multiply rocket launch system; visual prototype technology;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanic Automation and Control Engineering (MACE), 2011 Second International Conference on
Conference_Location
Hohhot
Print_ISBN
978-1-4244-9436-1
Type
conf
DOI
10.1109/MACE.2011.5987170
Filename
5987170
Link To Document