王玉惠
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Analysis of a MIMO Dutch roll dynamic system and its adaptive non-affine flight control
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Affiliation of Author(s):自动化学院

Journal:NONLINEAR DYNAMICS

Key Words:Dutch roll Non-affine Oscillation MIMO Adaptive

Abstract:Dutch roll motion is a type of aircraft lateral/directional oscillation, and its control problem has two main challenges. First, a multiple-input-multiple-output (MIMO) non-affine Dutch roll dynamics may result in nonzero equilibriums and unstable oscillations due to complex nonlinearities and disturbances. Second, the Dutch roll dynamical model is non-affine nonlinear, because it has nonlinear relationships not only with the state variables but also with the control inputs, which brings more difficulties to control it. Therefore, according to the analysis results of Dutch roll dynamics, a robust adaptive non-affine controller is designed to suppress the unstable oscillations with disturbances. Sliding mode method, fuzzy logic systems, and adaptive techniques are combined to construct the non-affine controller, without the need for the exact bound values of disturbances except for the theoretic proof. The simulation results show that the oscillations can be effectively suppressed using the proposed controller.

ISSN No.:0924-090X

Translation or Not:no

Date of Publication:2018-01-01

Co-author:Zhang, Jun

Correspondence Author:Wang Yuhui

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Professor
Supervisor of Doctorate Candidates

Gender:Female

Education Level:南京航空航天大学

Degree:Doctoral Degree in Engineering

School/Department:College of Automation Engineering

Discipline:Control Theory and Engineering. Control Science and Engineering

Business Address:自动化学院4号楼401

Contact Information:025-84892301-8023

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