Landing control system design for a flying-wing aircraft based on ADRC

Yanxiong Wang; Xiaoping Zhu; Zhou Zhou; Zhuang Shao

doi:10.1007/978-3-319-13966-1_34

Landing control system design for a flying-wing aircraft based on ADRC

Yanxiong Wang, Xiaoping Zhu, Zhou Zhou, Zhuang Shao

School of Aeronautics

Northwestern Polytechnical University Xian

Research output: Contribution to journal › Article › peer-review

4 Scopus citations

Abstract

In this paper, the flight simulation and control of a flying-wing aircraft in landing is presented. Significant dynamic nonlinearity and atmospheric disturbance are main problems for a flying-wing aircraft in landing phase. Therefore, a nonlinear controller with strong robustness is required. Active disturbance rejection control technique is used to design the controller which could estimate and compensate the uncertainties. A landing condition in which the wind shear encounters and ground effect before touchdown is considered, and a nonlinear longitudinal dynamic model of flying-wing aircraft in variable wind field is established. Simulations are conducted in MATLAB and the controller is shown to suppress the wind effects and ground proximity.

Original language	English
Pages (from-to)	340-351
Number of pages	12
Journal	Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
Volume	8917
DOIs	https://doi.org/10.1007/978-3-319-13966-1_34
State	Published - 2014

Keywords

Active disturbance rejection control
Control allocation
Flying-wing aircraft
Ground effect
Nonlinear control
Wind encounters

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10.1007/978-3-319-13966-1_34

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title = "Landing control system design for a flying-wing aircraft based on ADRC",

abstract = "In this paper, the flight simulation and control of a flying-wing aircraft in landing is presented. Significant dynamic nonlinearity and atmospheric disturbance are main problems for a flying-wing aircraft in landing phase. Therefore, a nonlinear controller with strong robustness is required. Active disturbance rejection control technique is used to design the controller which could estimate and compensate the uncertainties. A landing condition in which the wind shear encounters and ground effect before touchdown is considered, and a nonlinear longitudinal dynamic model of flying-wing aircraft in variable wind field is established. Simulations are conducted in MATLAB and the controller is shown to suppress the wind effects and ground proximity.",

keywords = "Active disturbance rejection control, Control allocation, Flying-wing aircraft, Ground effect, Nonlinear control, Wind encounters",

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AU - Wang, Yanxiong

AU - Zhu, Xiaoping

AU - Zhou, Zhou

AU - Shao, Zhuang

N1 - Publisher Copyright: © Springer International Publishing Switzerland 2014.

PY - 2014

Y1 - 2014

N2 - In this paper, the flight simulation and control of a flying-wing aircraft in landing is presented. Significant dynamic nonlinearity and atmospheric disturbance are main problems for a flying-wing aircraft in landing phase. Therefore, a nonlinear controller with strong robustness is required. Active disturbance rejection control technique is used to design the controller which could estimate and compensate the uncertainties. A landing condition in which the wind shear encounters and ground effect before touchdown is considered, and a nonlinear longitudinal dynamic model of flying-wing aircraft in variable wind field is established. Simulations are conducted in MATLAB and the controller is shown to suppress the wind effects and ground proximity.

AB - In this paper, the flight simulation and control of a flying-wing aircraft in landing is presented. Significant dynamic nonlinearity and atmospheric disturbance are main problems for a flying-wing aircraft in landing phase. Therefore, a nonlinear controller with strong robustness is required. Active disturbance rejection control technique is used to design the controller which could estimate and compensate the uncertainties. A landing condition in which the wind shear encounters and ground effect before touchdown is considered, and a nonlinear longitudinal dynamic model of flying-wing aircraft in variable wind field is established. Simulations are conducted in MATLAB and the controller is shown to suppress the wind effects and ground proximity.

KW - Active disturbance rejection control

KW - Control allocation

KW - Flying-wing aircraft

KW - Ground effect

KW - Nonlinear control

KW - Wind encounters

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JF - Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)

ER -

Landing control system design for a flying-wing aircraft based on ADRC

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