Sliding Mode Path following and Control Allocation of a Tilt-Rotor Quadcopter

A tilt-rotor quadcopter (TRQ) equipped with four tilt-rotors is more agile than its under-actuated counterpart and can fly at any path while maintaining the desired attitude. To take advantage of this additional control capability and enhance the quadrotor system’s robustness and capability, we desi...

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Main Authors: Chih-Chen Yih, Shih-Jeh Wu
Format: Article
Language:English
Published: MDPI AG 2022-11-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/12/21/11088
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author Chih-Chen Yih
Shih-Jeh Wu
author_facet Chih-Chen Yih
Shih-Jeh Wu
author_sort Chih-Chen Yih
collection DOAJ
description A tilt-rotor quadcopter (TRQ) equipped with four tilt-rotors is more agile than its under-actuated counterpart and can fly at any path while maintaining the desired attitude. To take advantage of this additional control capability and enhance the quadrotor system’s robustness and capability, we designed two sliding mode controls (SMCs): the typical SMC exploits the properties of the rotational dynamics, and the modified SMC avoids undesired chattering. Our simulation studies show that the proposed SMC scheme can follow the planned flight path and keep the desired attitude in the presence of variable deviations and external perturbations. We demonstrate from the Lyapunov stability theorem that the proposed control scheme can guarantee the asymptotic stability of the TRQ in terms of position and attitude following via control allocation.
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spelling doaj.art-2b552d0b36dd4849915c68392a8aef0b2023-11-24T03:37:51ZengMDPI AGApplied Sciences2076-34172022-11-0112211108810.3390/app122111088Sliding Mode Path following and Control Allocation of a Tilt-Rotor QuadcopterChih-Chen Yih0Shih-Jeh Wu1Department of Mechanical & Automation Engineering, I-Shou University, Kaohsiung 84001, TaiwanDepartment of Mechanical & Automation Engineering, I-Shou University, Kaohsiung 84001, TaiwanA tilt-rotor quadcopter (TRQ) equipped with four tilt-rotors is more agile than its under-actuated counterpart and can fly at any path while maintaining the desired attitude. To take advantage of this additional control capability and enhance the quadrotor system’s robustness and capability, we designed two sliding mode controls (SMCs): the typical SMC exploits the properties of the rotational dynamics, and the modified SMC avoids undesired chattering. Our simulation studies show that the proposed SMC scheme can follow the planned flight path and keep the desired attitude in the presence of variable deviations and external perturbations. We demonstrate from the Lyapunov stability theorem that the proposed control scheme can guarantee the asymptotic stability of the TRQ in terms of position and attitude following via control allocation.https://www.mdpi.com/2076-3417/12/21/11088tilt-rotor quadcopter (TRQ)sliding mode control (SMC)control allocationpath following
spellingShingle Chih-Chen Yih
Shih-Jeh Wu
Sliding Mode Path following and Control Allocation of a Tilt-Rotor Quadcopter
Applied Sciences
tilt-rotor quadcopter (TRQ)
sliding mode control (SMC)
control allocation
path following
title Sliding Mode Path following and Control Allocation of a Tilt-Rotor Quadcopter
title_full Sliding Mode Path following and Control Allocation of a Tilt-Rotor Quadcopter
title_fullStr Sliding Mode Path following and Control Allocation of a Tilt-Rotor Quadcopter
title_full_unstemmed Sliding Mode Path following and Control Allocation of a Tilt-Rotor Quadcopter
title_short Sliding Mode Path following and Control Allocation of a Tilt-Rotor Quadcopter
title_sort sliding mode path following and control allocation of a tilt rotor quadcopter
topic tilt-rotor quadcopter (TRQ)
sliding mode control (SMC)
control allocation
path following
url https://www.mdpi.com/2076-3417/12/21/11088
work_keys_str_mv AT chihchenyih slidingmodepathfollowingandcontrolallocationofatiltrotorquadcopter
AT shihjehwu slidingmodepathfollowingandcontrolallocationofatiltrotorquadcopter