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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Series: | International Journal of Advanced Robotic Systems |
Online Access: | https://doi.org/10.1177/1729881417699150 |
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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 |
work_keys_str_mv |
AT yangchen combinedoflyapunovstableandactivedisturbancerejectioncontrolforthepathfollowingofasmallunmannedaerialvehicle AT jianhongliang combinedoflyapunovstableandactivedisturbancerejectioncontrolforthepathfollowingofasmallunmannedaerialvehicle AT chaoleiwang combinedoflyapunovstableandactivedisturbancerejectioncontrolforthepathfollowingofasmallunmannedaerialvehicle AT yichengzhang combinedoflyapunovstableandactivedisturbancerejectioncontrolforthepathfollowingofasmallunmannedaerialvehicle |
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