Computing stability for autopilots based on vector margin

Jiang Wang*, De Fu Lin, Jun Fang Fan

*Corresponding author for this work

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

Abstract

A novel stability computation approach for tactical missile autopilots was detailed. The limitations of traditional stability margins were exhibited. Then the vector margin was introduced and examined. All available linear autopilot topologies were given and evaluated on the basis of vector margin. The analysis and computation results show that the presented method could give well description for control system stability.

Original languageEnglish
Title of host publicationFuture Control and Automation - Proceedings of the 2nd International Conference on Future Control and Automation, ICFCA 2012
Pages455-460
Number of pages6
EditionVOL. 2
DOIs
Publication statusPublished - 2012
Event2nd International Conference on Future Control and Automation, ICFCA 2012 - Changsha, China
Duration: 1 Jul 20122 Jul 2012

Publication series

NameLecture Notes in Electrical Engineering
NumberVOL. 2
Volume173 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

Conference2nd International Conference on Future Control and Automation, ICFCA 2012
Country/TerritoryChina
CityChangsha
Period1/07/122/07/12

Keywords

  • autopilot
  • stability computation
  • vector margin

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