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Research of trajectory tracking control of cruise missile based on observer

  • Beihang University

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

Abstract

To achieve cruise missile accurate trajectory tracking control, an observer-based tracking control method is designed. An observer is developed to estimate the states and control signals of desired trajectory as the inputs of the tracking controller. The linear quadratic optimal control is used to realize full-state feedback control for trajectory tracking. A certain cruise missile is used for the tracking simulation and the result shows satisfactory performance, the control method is simple and suitable for engineering applications.

Original languageEnglish
Title of host publicationFrontiers of Mechanical Engineering and Materials Engineering
Pages1599-1602
Number of pages4
DOIs
StatePublished - 2012
Event2012 International Conference on Frontiers of Mechanical Engineering and Materials Engineering, MEME 2012 - Hong Kong, Hong Kong SAR
Duration: 27 Jul 201229 Jul 2012

Publication series

NameApplied Mechanics and Materials
Volume184-185
ISSN (Print)1660-9336
ISSN (Electronic)1662-7482

Conference

Conference2012 International Conference on Frontiers of Mechanical Engineering and Materials Engineering, MEME 2012
Country/TerritoryHong Kong SAR
CityHong Kong
Period27/07/1229/07/12

Keywords

  • Cruise missile
  • Observer
  • Quadratic optimal control
  • Trajectory tracking

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