Influence of revolving angle measure precision and actuator performance on control force

Yan Chao Bi, Xiao Xian Yao, Xiao Dong Song

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

1 Citation (Scopus)

Abstract

A control mathematical model in pitch and yaw direction is presented to apply on missiles controlled by double-channel with' + ' style canard. Based on the mathematical model, the influence of deflection angle measurement error and actuator performance on actuator control is analyzed. The results show that the measure error of lean angle and actuator delay will produce control coupling in pitch and yaw direction and that will reduce control efficiency.

Original languageEnglish
Title of host publicationMaterials Technologies, Automation Systems and Information Technologies in Industry
Pages765-769
Number of pages5
DOIs
Publication statusPublished - 2013
Event2013 International Conference on Mechatronic Systems and Materials Application, ICMSMA 2013 - Guangzhou, China
Duration: 26 Jun 201327 Jun 2013

Publication series

NameApplied Mechanics and Materials
Volume389
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2013 International Conference on Mechatronic Systems and Materials Application, ICMSMA 2013
Country/TerritoryChina
CityGuangzhou
Period26/06/1327/06/13

Keywords

  • Actuator
  • Guided projectile
  • Missile control
  • Rolling missile

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