Rapid design of guidance and control loop for laser guided bomb

Meihong Li, Jian Yin, Jingzhang Wang, Jinxiang Xu

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

Abstract

The purpose of this research is to propose a rapid design of guidance and control loop for laser guided bomb. Aerodynamic parameters which are difficult to obtain fast at the beginning of design, are calculated by Missile Datcom software. Then every parameter of missile body transfer function is achieved and precious transfer function is determined. Furthermore, pitching stability loop, side stability loop, roll stability loop and gravity compensation loop are built. Then all the designed loops and target practice are simulated in Matlab/Simulink, and the results demonstrate that the design is correct and effective.

Original languageEnglish
Title of host publicationProceedings of the 32nd Chinese Control Conference, CCC 2013
PublisherIEEE Computer Society
Pages5620-5625
Number of pages6
ISBN (Print)9789881563835
Publication statusPublished - 18 Oct 2013
Event32nd Chinese Control Conference, CCC 2013 - Xi'an, China
Duration: 26 Jul 201328 Jul 2013

Publication series

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

Conference

Conference32nd Chinese Control Conference, CCC 2013
Country/TerritoryChina
CityXi'an
Period26/07/1328/07/13

Keywords

  • Gravity compensation
  • Missile Datcom
  • Stability loop
  • Transfer function

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