Quadrotor UAV: collision resilience behaviors

In this article, a safety control scheme for quadrotor is proposed to guarantee collision resilience like flying insects. The direction and magnitude of contact wrench are quantitatively analyzed subject to the compliant contact wrench model. A nonlinear disturbance observer is developed to estimate...

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Main Authors: Fan, Dadong, Guo, Kexin, Lyu, Shangke, Yu, Xiang, Xie, Lihua, Guo, Lei
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2023
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Online Access:https://hdl.handle.net/10356/170683
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1706832023-09-26T01:28:43Z Quadrotor UAV: collision resilience behaviors Fan, Dadong Guo, Kexin Lyu, Shangke Yu, Xiang Xie, Lihua Guo, Lei School of Electrical and Electronic Engineering Engineering::Electrical and electronic engineering Collision Resilience Nonlinear Disturbance Observer In this article, a safety control scheme for quadrotor is proposed to guarantee collision resilience like flying insects. The direction and magnitude of contact wrench are quantitatively analyzed subject to the compliant contact wrench model. A nonlinear disturbance observer is developed to estimate the contact wrench exerted on the quadrotor, and effective collision detection can be guaranteed based on the observer. Subsequently, a tilt-torsion decomposition-based attitude controller is developed to prioritize the correction of horizontal posture over yaw error. The attitude error is separated into roll-pitch portion and yaw portion. Reasonable roll and pitch torques can be generated by allocating a higher gain for roll-pitch portion, allowing the quadrotor to recover from collisions promptly. Simulations and flight experiments are carried out to demonstrate the effectiveness of the proposed collision resilience control scheme. This work was supported in part by the National Key Research and Development Program of China under Grant 2020YFA0711200, in part by the National Natural Science Foundation of China under Grant 62273023, Grant 61903019, and Grant 61973012, in part by the Defense Industrial Technology Development Program under Grant JCKY2020601C016, in part by the Program for Changjiang Scholars and Innovative Research Team (IRT 16R03), in part by the Key Research and Development Program of Zhejiang under Grant 2021C03158, in part by the Science and Technology Key Innovative Project of Hangzhou under Grant 20182014B06 and Grant 2022AIZD0137, Zhejiang Provincial Natural Science Foundation under Grant LQ20F030006, and in part by Zhejiang Lab under Grant 2019NB0AB08. 2023-09-26T01:28:43Z 2023-09-26T01:28:43Z 2023 Journal Article Fan, D., Guo, K., Lyu, S., Yu, X., Xie, L. & Guo, L. (2023). Quadrotor UAV: collision resilience behaviors. IEEE Transactions On Aerospace and Electronic Systems, 59(3), 2092-2104. https://dx.doi.org/10.1109/TAES.2022.3211479 0018-9251 https://hdl.handle.net/10356/170683 10.1109/TAES.2022.3211479 2-s2.0-85162367452 3 59 2092 2104 en IEEE Transactions on Aerospace and Electronic Systems © 2022 IEEE. All rights reserved.
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Electrical and electronic engineering
Collision Resilience
Nonlinear Disturbance Observer
spellingShingle Engineering::Electrical and electronic engineering
Collision Resilience
Nonlinear Disturbance Observer
Fan, Dadong
Guo, Kexin
Lyu, Shangke
Yu, Xiang
Xie, Lihua
Guo, Lei
Quadrotor UAV: collision resilience behaviors
description In this article, a safety control scheme for quadrotor is proposed to guarantee collision resilience like flying insects. The direction and magnitude of contact wrench are quantitatively analyzed subject to the compliant contact wrench model. A nonlinear disturbance observer is developed to estimate the contact wrench exerted on the quadrotor, and effective collision detection can be guaranteed based on the observer. Subsequently, a tilt-torsion decomposition-based attitude controller is developed to prioritize the correction of horizontal posture over yaw error. The attitude error is separated into roll-pitch portion and yaw portion. Reasonable roll and pitch torques can be generated by allocating a higher gain for roll-pitch portion, allowing the quadrotor to recover from collisions promptly. Simulations and flight experiments are carried out to demonstrate the effectiveness of the proposed collision resilience control scheme.
author2 School of Electrical and Electronic Engineering
author_facet School of Electrical and Electronic Engineering
Fan, Dadong
Guo, Kexin
Lyu, Shangke
Yu, Xiang
Xie, Lihua
Guo, Lei
format Article
author Fan, Dadong
Guo, Kexin
Lyu, Shangke
Yu, Xiang
Xie, Lihua
Guo, Lei
author_sort Fan, Dadong
title Quadrotor UAV: collision resilience behaviors
title_short Quadrotor UAV: collision resilience behaviors
title_full Quadrotor UAV: collision resilience behaviors
title_fullStr Quadrotor UAV: collision resilience behaviors
title_full_unstemmed Quadrotor UAV: collision resilience behaviors
title_sort quadrotor uav: collision resilience behaviors
publishDate 2023
url https://hdl.handle.net/10356/170683
_version_ 1779156463725314048