Self-Scheduled and Robust Control for Tilt Rotor Aircraft

Yu Yan Cao; Xin Min Wang; Cheng Peng

doi:10.4028/www.scientific.net/AMM.721.210

Paper Titles

Modeling and Simulation of a New Type Intelligent Gas Pressure Regulator
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Calculation on Fracture Parameter of Model I Crack Tip Based on ANSYS
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Three-Dimensional Numerical Simulation of the Flow around Two Side-by-Side Cylinders of Different Diameters
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Particle Swarm Optimization of PI^λD^μ Control of Heating Furnace Temperature Control System
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Self-Scheduled and Robust Control for Tilt Rotor Aircraft
p.210

Mathematical Model of Obstacle Avoidance Shortest Time Path for Robot
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Synchronization Control of Chaotic Systems with Different Orders
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Research on Carrier-Attacker Control before Launching Air-Ground Guidance Weapons
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Control of Channel Power Compensation Based on Genetic Algorithm to Impairment Aware in Optical Network
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 721Self-Scheduled and Robust Control for Tilt Rotor...

Self-Scheduled and Robust Control for Tilt Rotor Aircraft

Abstract:

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.

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Periodical:

Applied Mechanics and Materials (Volume 721)

Pages:

210-213

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.721.210

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Online since:

December 2014

Authors:

Yu Yan Cao*, Xin Min Wang, Cheng Peng

Keywords:

Convex Combination, Robust, Self-Scheduled

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* - Corresponding Author

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