Design of augmentation stability control system for hovering of ducted propeller air vehicle

Ming Xi Li*, Chang Le Xiang, Yue Ma, Lijun Zhu, Bin Xu

*Corresponding author for this work

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

Abstract

The aerodynamic dynamic model of hovering for air vehicle with longitudinal double ducted propeller is established by analysis aerodynamic characteristics, Relative gain array of various channels is calculated to evaluate the coupling degree among various channels, Decoupling control matrix and stability augmentation control system is designed. The empirical data on scaled model shows that air vehicle could hover stably and be in good agreement with the design goal.

Original languageEnglish
Title of host publicationProceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012
Pages873-877
Number of pages5
Publication statusPublished - 2012
Event2012 International Conference on Modelling, Identification and Control, ICMIC 2012 - Wuhan, China
Duration: 24 Jun 201226 Jun 2012

Publication series

NameProceedings of 2012 International Conference on Modelling, Identification and Control, ICMIC 2012

Conference

Conference2012 International Conference on Modelling, Identification and Control, ICMIC 2012
Country/TerritoryChina
CityWuhan
Period24/06/1226/06/12

Keywords

  • Air Vehicle
  • Decoupling Control
  • Stability

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