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Missile stage separation simulation considering complex factors

  • Harbin Institute of Technology

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

In this paper, a kinematics and dynamic model of missile stage cold separation process is established. The stage separation of missile is simulated considering the influence of separation motor thrust bias and residual thrust point bias and thrust direction deflection of spent stage. Separate bodies' movement despite deviation interference is obtained. Moreover, Monte-Carlo method is also used to analyzing the range of separation bodies' movement. These results provide a reference for missile separation simulation and interference factors analysis.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control Conference, CCC 2015
EditorsQianchuan Zhao, Shirong Liu
PublisherIEEE Computer Society
Pages8768-8772
Number of pages5
ISBN (Electronic)9789881563897
DOIs
StatePublished - 11 Sep 2015
Event34th Chinese Control Conference, CCC 2015 - Hangzhou, China
Duration: 28 Jul 201530 Jul 2015

Publication series

NameChinese Control Conference, CCC
Volume2015-September
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference34th Chinese Control Conference, CCC 2015
Country/TerritoryChina
CityHangzhou
Period28/07/1530/07/15

Keywords

  • Complex factors
  • Monte-Carlo method
  • Simulation
  • Stage separation

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