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Modeling and simulation of the helicopter control system based on the flight qualities

  • Cheng Wen Jian*
  • , Shu Li
  • , J. Zhang
  • *Corresponding author for this work
  • Beihang University

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

Abstract

Helicopter is a strong coupling and instability nonlinear system, of which the inherent flight qualities are poor. Helicopter model following control technology can make four control channels of helicopter with excellent tracking and decoupling characteristics. This paper applied the control method of model following control combining eigenststructure assignment to the helicopter control system. The results of simulation show that the helicopter flight qualities meet the requirements of ADS-33, the helicopter has excellent tracking and decoupling characteristics. Thus it proves that this control method is of great effectiveness.

Original languageEnglish
Title of host publicationMaterials, Transportation and Environmental Engineering II
EditorsJimmy C.M. Kao, Wen-Pei Sung, Ran Chen
PublisherTrans Tech Publications Ltd
Pages1493-1497
Number of pages5
ISBN (Electronic)9783038352488
DOIs
StatePublished - 2014
Event2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 - Kunming, China
Duration: 30 Jul 201431 Jul 2014

Publication series

NameAdvanced Materials Research
Volume1030-1032
ISSN (Print)1022-6680
ISSN (Electronic)1662-8985

Conference

Conference2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014
Country/TerritoryChina
CityKunming
Period30/07/1431/07/14

Keywords

  • Eigenststructure assignment
  • Flight control
  • Flight qualities
  • Helicopter
  • Model following control

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