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Modeling and simulation of the interceptor by combined control of lateral thrust and aerodynamic force

  • Yin Yongxin*
  • , Yang Ming
  • , Wang Zicai
  • *Corresponding author for this work
  • Harbin Institute of Technology

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

Abstract

Nonlinear dynamic model and kinetic model are constructed based on the moment of momentum theorem for the interceptor by combined control, and a model of the impulse motor is presented. These models can precisely describe the motion of the interceptor when the interceptor is controlled by combined control and aerodynamic force, respectively. A model of the relative movement between the target and interceptor is also constructed, which is useful to control interceptor and is convenient for the practical project. The simulation results show that these models have satisfactory control precision for small or large attitude maneuver of the interceptor, and have satisfactory guiding precision for non-maneuverable or maneuverable target also, which shows the veracity and advantage.

Original languageEnglish
Title of host publicationProceedings of the World Congress on Intelligent Control and Automation (WCICA)
Pages1805-1809
Number of pages5
DOIs
StatePublished - 2006
Event6th World Congress on Intelligent Control and Automation, WCICA 2006 - Dalian, China
Duration: 21 Jun 200623 Jun 2006

Publication series

NameProceedings of the World Congress on Intelligent Control and Automation (WCICA)
Volume1

Conference

Conference6th World Congress on Intelligent Control and Automation, WCICA 2006
Country/TerritoryChina
CityDalian
Period21/06/0623/06/06

Keywords

  • Combined control
  • Impulse motor
  • Interceptor
  • Lateral thrust
  • Modeling

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