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Open AccessJournal ArticleDOI

Gain self-scheduled H∞ control for morphing aircraft in the wing transition process based on an LPV model

Ting Yue, +2 more
- 01 Aug 2013 - 
- Vol. 26, Iss: 4, pp 909-917
TLDR
In this paper, the authors investigated gain self-scheduled H∞ robust control system design for a tailless folding-wing morphing aircraft in the wing shape varying process.
About
This article is published in Chinese Journal of Aeronautics.The article was published on 2013-08-01 and is currently open access. It has received 63 citations till now. The article focuses on the topics: Morphing & Wing.

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Citations
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Journal ArticleDOI

Modified adaptive neural dynamic surface control for morphing aircraft with input and output constraints

TL;DR: In this paper, a barrier Lyapunov function-based adaptive neural dynamic surface control approach is proposed for morphing aircraft subject to unknown parameters and input-output constraints, which can ensure good tracing performance of the aircraft in the fixed configuration and morphing process.
Journal ArticleDOI

A systematic method of smooth switching LPV controllers design for a morphing aircraft

TL;DR: In this article, a smooth switching linear parameter-varying (LPV) controller design for a morphing aircraft with a variable wing sweep angle is presented, and a systematic algorithm is developed to improve the efficiency of the controllers design process.
Journal ArticleDOI

Morphing aircraft control based on switched nonlinear systems and adaptive dynamic programming

TL;DR: This paper investigates the control problem of a morphing aircraft with variable sweep wings based on switched nonlinear systems and adaptive dynamic programming (ADP) and proposes an ADP approach with the name of action-dependent heuristic dynamic programming to decrease the altitude tracking error.
References
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Journal ArticleDOI

A simplex method for function minimization

TL;DR: A method is described for the minimization of a function of n variables, which depends on the comparison of function values at the (n 41) vertices of a general simplex, followed by the replacement of the vertex with the highest value by another point.
Book

Aircraft Control and Simulation

TL;DR: Equations of Motion Building the Aircraft Model Basic Analytical and Computational Tools Aircraft Dynamics and Classical Design Techniques Modern Design Techniques Robustness and Multivariable Frequency-Domain Techniques Digital Control Appendices Index.
Journal ArticleDOI

Self-scheduled H ∞ control of linear parameter-varying systems: a design example

TL;DR: The methodology presented in this paper is applied to the gain scheduling of a missile autopilot and is to bypass most difficulties associated with more classical schemes such as gain-interpolation or gain-scheduling techniques.
Journal ArticleDOI

Development of linear-parameter-varying models for aircraft

TL;DR: In this article, a comparative study of three linear-parameter-varying (LPV) modeling approaches and their application to the longitudinal motion of a Boeing 747 series 100/200 is presented.
Proceedings ArticleDOI

The Aircraft Morphing Program

TL;DR: The NASA Aircraft Morphing program as mentioned in this paper is an attempt to couple research across a wide range of disciplines to integrate smart technologies into high payoff aircraft applications, and the program bridges research in seven individual disciplines and combines the effort into activities in three primary program thrusts.
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