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Engineering modeling and simulation for new estimation of aircraft's dynamic angles

  • Zhao Wu*
  • , Lixin Wang
  • *Corresponding author for this work
  • Beihang University

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

Abstract

The measurement of aircraft's dynamic angles is difficult and inaccurate due to the precarious flight environment. This paper brings forward and amends a new estimation of aircraft's angle of attack and sideslip angle based on the basic of INS/GPS data. Through engineering modeling of closed-loop flight simulation framework and estimation method, the result shows obvious rationality and veracity.

Original languageEnglish
Title of host publicationSystem Simulation and Scientific Computing - International Conference, ICSC 2012, Proceedings
Pages112-117
Number of pages6
EditionPART 1
DOIs
StatePublished - 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

  • Angle of Attack
  • INS/GPS
  • Modeling
  • Pilot model
  • Sideslip Angle

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