Optimal robust control for attitude of quad-rotor aircraft based on SDRE

Jing Liang Sun, Chun Sheng Liu, Ke Lu, Hao Ming Shi

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

9 Citations (Scopus)

Abstract

The attitude control is the key of the automatic flight for a quad-rotor aircraft. In order to guarantee the robustness of the quad-rotor aircraft for various uncertainties, a new design method of the robust optimal control that integrates the sliding mode control theory with state-dependent Riccati equation (SDRE) is proposed in this paper. First, the whole attitude kinematical model is obtained. By using the SDRE approach, an optimal control law of the attitude for quad-rotor aircraft without uncertainties is obtained. Then, the sliding mode control theory combing with SDRE is applied to improve the robustness of the quad-rotor aircraft. As a result, the system is robust optimal to the parameters variations or extraneous disturbances and the stability is proved. Finally, the validity and robustness of the proposed algorithm are verified by simulation results.

Original languageEnglish
Title of host publicationProceedings of the 34th Chinese Control Conference, CCC 2015
EditorsQianchuan Zhao, Shirong Liu
PublisherIEEE Computer Society
Pages2333-2337
Number of pages5
ISBN (Electronic)9789881563897
DOIs
Publication statusPublished - 11 Sept 2015
Externally publishedYes
Event34th Chinese Control Conference, CCC 2015 - Hangzhou, China
Duration: 28 Jul 201530 Jul 2015

Publication series

NameChinese Control Conference, CCC
Volume2015-September
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference34th Chinese Control Conference, CCC 2015
Country/TerritoryChina
CityHangzhou
Period28/07/1530/07/15

Keywords

  • quad-rotor
  • sliding mode
  • state-dependent Riccati equation (SDRE)
  • uncertainty

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