Longitudinal displacement autopilot design for Boeing 747-400 by root-locus

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

Abstract

In this paper, displacement autopilot has been designed for Boeing 747-400 and appropriate Samp and Srg values have been obtained. Moreover root locus diagrams are also drawn. Finally pitch angle time response is analyzed.

Original languageEnglish
Title of host publicationProceedings of the 9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07
Pages87-92
Number of pages6
Publication statusPublished - 2007
Event9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07 - Istanbul, Turkey
Duration: 27 May 200729 May 2007

Publication series

NameProceedings of the 9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07

Conference

Conference9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07
Country/TerritoryTurkey
CityIstanbul
Period27/05/0729/05/07

Keywords

  • Boeing 747-400
  • Displacement autopilots
  • Root-locus design

Fingerprint

Dive into the research topics of 'Longitudinal displacement autopilot design for Boeing 747-400 by root-locus'. Together they form a unique fingerprint.

Cite this