Design and analysis of missile two-loop autopilot with angle of attack feedback

Jiang Wang*, Zhe Yang, De Fu Lin

*Corresponding author for this work

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

2 Citations (Scopus)

Abstract

In order to eliminate the static error of the classic two loop autopilot, the PI compensator is introduced into the control system. To enhance the robustness of two loop autopilot with PI compensator, an angle of attack feedback is introduced into the system. Using the method of pole-place, the controller parameters of different two loop autopilot topologies are deduced. The analytical results show that a well designed two-loop autopilot with PI compensator can introduce a zero in numerator which counteracts the first-order inertial loop in denominator. However, the two-loop autopilot with PI compensator and angle of attack feedback introduces the phase-lead compensation in the feedback-loop. The zero cannot cancel the first-order inertial loop in denominator, and it is dominated by the first-order inertial loop. This kind of autopilot topology has better robustness than others.

Original languageEnglish
Title of host publicationSystem Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings
Pages287-296
Number of pages10
EditionPART 1
DOIs
Publication statusPublished - 2012
EventAsia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012 - Shanghai, China
Duration: 27 Oct 201230 Oct 2012

Publication series

NameCommunications in Computer and Information Science
NumberPART 1
Volume326 CCIS
ISSN (Print)1865-0929

Conference

ConferenceAsia Simulation Conference and the International Conference on System Simulation and Scientific Computing 2012, AsiaSim and ICSC 2012
Country/TerritoryChina
CityShanghai
Period27/10/1230/10/12

Keywords

  • PI compensator
  • angle of attack feedback
  • missile
  • two loop autopilot

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