Title :
Dynamic simulation of rocket launch system based on virtual prototype technology
Author_Institution :
Eng. Coll., Liyin Univ., Linyi, China
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;
Conference_Titel :
Mechanic Automation and Control Engineering (MACE), 2011 Second International Conference on
Conference_Location :
Hohhot
Print_ISBN :
978-1-4244-9436-1
DOI :
10.1109/MACE.2011.5987170
