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

Volume

2

fYear

2011

fDate

22-23 Oct. 2011

Firstpage

97

Lastpage

100

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;

fLanguage

English

Publisher

ieee

Conference_Titel

System Science, Engineering Design and Manufacturing Informatization (ICSEM), 2011 International Conference on

Conference_Location

Guiyang

Print_ISBN

978-1-4577-0247-1

Type

conf

DOI

10.1109/ICSSEM.2011.6081339

Filename

6081339