Title :
Comparative analysis of two option of separating engine of precision guided rocket
Author :
Xu, Jingqing ; Qi, Xinglin ; Wang, Junbo ; Jiao, Jianshe
Author_Institution :
Ordnance Eng. Coll., Shijiazhuang, China
Abstract :
Range and separating stability is comparing and analyzing in connection with two plan of separating engine of precision guided rocket. The mathematic model of boost phase and free flight phase is built, and the simulation model is design by MATLAB/Simulink. The trajectory is simulated, and the range is obtained when the angle of fire and the separation speed. The result says that the range scope option one is larger than option two, but the two options is all satisfied the range target. But the separation stability of option two is better than option one, so option two is fit to precision guided rocket.
Keywords :
precision engineering; rocket engines; angle of fire; boost phase; comparative analysis; mathematic model; precision guided rocket; range scope option; range target; separating engine; separation speed; separation stability; MATLAB; Navigation; precision guided rocket; range; separation stability; trajectory simulation;
Conference_Titel :
System Science, Engineering Design and Manufacturing Informatization (ICSEM), 2011 International Conference on
Conference_Location :
Guiyang
Print_ISBN :
978-1-4577-0247-1
DOI :
10.1109/ICSSEM.2011.6081339
