Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle

This article proposes a composite path following controller that allows the small fixed-wing unmanned aerial vehicle to follow a predefined path. Assuming that the vehicle is equipped with an autopilot for altitude and airspeed maintained well, the controller design adopts the hierarchical control s...

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Main Authors: Yang Chen, Jianhong Liang, Chaolei Wang, Yicheng Zhang
Format: Article
Language:English
Published: SAGE Publishing 2017-03-01
Series:International Journal of Advanced Robotic Systems
Online Access:https://doi.org/10.1177/1729881417699150
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spelling doaj-b34ca137f9614a1c97f4774ae926c27e2020-11-25T03:32:21ZengSAGE PublishingInternational Journal of Advanced Robotic Systems1729-88142017-03-011410.1177/172988141769915010.1177_1729881417699150Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicleYang Chen0Jianhong Liang1Chaolei Wang2Yicheng Zhang3 School of Mechanical and Electrical Engineering, Longyan University, Longyan, Fujian, China Robotics Institute, Beihang University, Beijing, China Science and Technology on Special System Simulation Laboratory, Beijing Simulation Center, Beijing, China Robotics Institute, Beihang University, Beijing, ChinaThis article proposes a composite path following controller that allows the small fixed-wing unmanned aerial vehicle to follow a predefined path. Assuming that the vehicle is equipped with an autopilot for altitude and airspeed maintained well, the controller design adopts the hierarchical control structure. With the inner-loop controller design based on the notion of active disturbance rejection control which will respond to the desired roll angle command, the core part of the outer-loop controller is designed based on Lyapunov stability theorem to generate the desired course rate for the straight-line paths. The bank to turn maneuver is used to transform the desired course rate to the desired roll angle command. Both the hardware-in-the-loop simulation in the X-Plane simulator and actual experimental flight tests have been successfully achieved, which verified the effectiveness of the proposed method.https://doi.org/10.1177/1729881417699150
collection DOAJ
language English
format Article
sources DOAJ
author Yang Chen
Jianhong Liang
Chaolei Wang
Yicheng Zhang
spellingShingle Yang Chen
Jianhong Liang
Chaolei Wang
Yicheng Zhang
Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle
International Journal of Advanced Robotic Systems
author_facet Yang Chen
Jianhong Liang
Chaolei Wang
Yicheng Zhang
author_sort Yang Chen
title Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle
title_short Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle
title_full Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle
title_fullStr Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle
title_full_unstemmed Combined of Lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle
title_sort combined of lyapunov-stable and active disturbance rejection control for the path following of a small unmanned aerial vehicle
publisher SAGE Publishing
series International Journal of Advanced Robotic Systems
issn 1729-8814
publishDate 2017-03-01
description This article proposes a composite path following controller that allows the small fixed-wing unmanned aerial vehicle to follow a predefined path. Assuming that the vehicle is equipped with an autopilot for altitude and airspeed maintained well, the controller design adopts the hierarchical control structure. With the inner-loop controller design based on the notion of active disturbance rejection control which will respond to the desired roll angle command, the core part of the outer-loop controller is designed based on Lyapunov stability theorem to generate the desired course rate for the straight-line paths. The bank to turn maneuver is used to transform the desired course rate to the desired roll angle command. Both the hardware-in-the-loop simulation in the X-Plane simulator and actual experimental flight tests have been successfully achieved, which verified the effectiveness of the proposed method.
url https://doi.org/10.1177/1729881417699150
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AT chaoleiwang combinedoflyapunovstableandactivedisturbancerejectioncontrolforthepathfollowingofasmallunmannedaerialvehicle
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