A predictive research for the range of hood separation and landing locations considering multiple factors

Author

Huitong Li ; Yang Zhao ; Yixin Huang ; Hao Tian

Author_Institution

Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China

fYear

2015

fDate

2-5 Aug. 2015

Firstpage

664

Lastpage

669

Abstract

The separation process of missile hood is influenced by many kinds of uncertain factors, along with limited trial number of target range and interplay between influencing factors, thus it is difficult to precisely determine separation process and hood landing locations. The aim of this study is to establish dynamic simulation model of hood separation and landing track based on Monte-Carlo method. From repeated digital simulation calculations considering many influential factors, statistics parameters of landing location are obtained. This study provides a technical support for facilities protection on launching site.

Keywords

Monte Carlo methods; missile guidance; Monte-Carlo method; digital simulation; dynamic simulation model; facility protection; hood landing locations; influencing factors; landing track; launching site; missile hood separation process; predictive research; statistics parameters; target range; uncertain factors; Aerodynamics; Engines; Force; Mathematical model; Missiles; Monte Carlo methods; Separation processes; Hood separation; Landing locations; Monte-Carlo method;

fLanguage

English

Publisher

ieee

Conference_Titel

Mechatronics and Automation (ICMA), 2015 IEEE International Conference on

Conference_Location

Beijing

Print_ISBN

978-1-4799-7097-1

Type

conf

DOI

10.1109/ICMA.2015.7237564

Filename

7237564