Design for Automatic Landing Flight Control Law Based on Active Disturbance Rejection Control Method

ZHANG Xiang; LI Guangwen; CAO Ruiting; XUE Guanglong

doi:10.15892/j.cnki.djzdxb.2020.05.024

Journal of Projectiles, Rockets, Missiles and Guidance >

2020 , Vol. 40 >Issue 5: 98 - 104

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2020.05.024

Design for Automatic Landing Flight Control Law Based on Active Disturbance Rejection Control Method

ZHANG Xiang ¹ ,
LI Guangwen ¹ ,
CAO Ruiting ² ,
XUE Guanglong ³

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¹ School of Automation, Northwestern Polytechnical University, Xi’an 710072, China
² Xi’an Flight Automatic Control Research Institute, Xi’an 710065, China
³ China National Aeronautical Radio Electronics Research Institute, Shanghai 200233, China

Received date: 2019-10-25

Online published: 2025-05-30

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Abstract

In order to solve the anti-disturbance problem of aircraft landing control under strong disturbance, a design method of attitude and automatic throttle control law based on active disturbance rejection control method was given in this paper. In the active disturbance rejection control theory, if the nonlinear fal function is not smooth, the controller oscillation problem is induced at the subsection point, in this paper, the nonlinear function is reconstructed by using the continuous and derivable condition, by this method, the controller performance is improved. Taking a transport aircraft as an object, the automatic landing simulation is carried out under the condition of turbulence disturbance and parameter perturbation. The simulation results show that automatic landing control law designed by the active disturbance rejection method has good robustness.

Key words： attitude control; automatic throttle; active disturbance rejection; robustness

Cite this article

ZHANG Xiang , LI Guangwen , CAO Ruiting , XUE Guanglong . Design for Automatic Landing Flight Control Law Based on Active Disturbance Rejection Control Method[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2020 , 40(5) : 98 -104 . DOI: 10.15892/j.cnki.djzdxb.2020.05.024

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