Self-Scheduled and Robust Control for Tilt Rotor Aircraft

A kind of self-scheduled and robust control algorithm for the conversion mode of tilt rotor aircraft is proposed in this paper. The mathematical model of the aircraft is established by modeling each component and combining. Then the conversion corridor is obtained by trim results. The convex combina...

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Bibliographic Details
Published inApplied Mechanics and Materials Vol. 721; no. Vehicle, Mechanical and Electrical Engineering; pp. 210 - 213
Main Authors Peng, Cheng, Wang, Xin Min, Cao, Yu Yan
Format Journal Article
LanguageEnglish
Published Zurich Trans Tech Publications Ltd 01.12.2014
Subjects
Aircraft components
Conversion
Corridors
Interpolation
Mathematical models
Matlab
Robust control
Tilt rotor aircraft
Convex Combination
Self-Scheduled
Robust
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Summary:A kind of self-scheduled and robust control algorithm for the conversion mode of tilt rotor aircraft is proposed in this paper. The mathematical model of the aircraft is established by modeling each component and combining. Then the conversion corridor is obtained by trim results. The convex combination of several vertex system combined with two-dimensional interpolation is designed to solve the problem of self-scheduled while nacelle tilting. Last sufficient and necessary conditions for the existence of the state-feedback controller are given and a MATLAB tool is raised to ensure performance of the system.
Bibliography:Selected, peer reviewed papers from the 2014 International Conference on Vehicle, Mechanical and Electrical Engineering (ICVMEE 2014), November 29-30, 2014, Wuhan, China
ObjectType-Article-1
SourceType-Scholarly Journals-1
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ISBN:3038353833
9783038353836
ISSN:1660-9336
1662-7482
1662-7482
DOI:10.4028/www.scientific.net/AMM.721.210