Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure Conditions

This paper aims to propose a strategy for the flight control of quad-rotors under single rotor failure conditions. The proposed control strategy consists of two stages—fault detection (FD) and fault tolerant control (FTC). A dual observer-based strategy for FD and fault estimation is developed. With...

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Main Authors: Yu-Hsuan Lien, Chao-Chung Peng, Yi-Hsuan Chen
Format: Article
Language:English
Published: MDPI AG 2020-05-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/10/10/3503
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spelling doaj-e3fa89b818d94306bc650c9531ea93832020-11-25T02:04:06ZengMDPI AGApplied Sciences2076-34172020-05-01103503350310.3390/app10103503Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure ConditionsYu-Hsuan Lien0Chao-Chung Peng1Yi-Hsuan Chen2Department of Aeronautics and Astronautics, National Cheng Kung University, Tainan 701, TaiwanDepartment of Aeronautics and Astronautics, National Cheng Kung University, Tainan 701, TaiwanDepartment of Aeronautics and Astronautics, National Cheng Kung University, Tainan 701, TaiwanThis paper aims to propose a strategy for the flight control of quad-rotors under single rotor failure conditions. The proposed control strategy consists of two stages—fault detection (FD) and fault tolerant control (FTC). A dual observer-based strategy for FD and fault estimation is developed. With the combination of the results from both observers, the decision making in whether a fault actually happened or the observed anomaly was caused by an external disturbance could be distinguished. Following the FD result, a control strategy for normal flight, as well as the abnormal one, is presented. The FTC considers a real-time coordinate transformation scheme to manipulate the target angles for the quad-rotor to follow a prescribed trajectory. When a rotor fault happens, it is going to be detected by the dual observers and then the FTC is activated to stabilize the system such that the trajectory following task can still be fulfilled. Furthermore, in order to achieve robust flight in the presence of external wind perturbation, the sliding mode control (SMC) theory is further integrated. Simulations illustrate the effectiveness and feasibility of the proposed method.https://www.mdpi.com/2076-3417/10/10/3503quadrotoractuator faultfault detectionfault tolerant controlsliding mode control
collection DOAJ
language English
format Article
sources DOAJ
author Yu-Hsuan Lien
Chao-Chung Peng
Yi-Hsuan Chen
spellingShingle Yu-Hsuan Lien
Chao-Chung Peng
Yi-Hsuan Chen
Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure Conditions
Applied Sciences
quadrotor
actuator fault
fault detection
fault tolerant control
sliding mode control
author_facet Yu-Hsuan Lien
Chao-Chung Peng
Yi-Hsuan Chen
author_sort Yu-Hsuan Lien
title Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure Conditions
title_short Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure Conditions
title_full Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure Conditions
title_fullStr Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure Conditions
title_full_unstemmed Adaptive Observer-Based Fault Detection and Fault-Tolerant Control of Quadrotors under Rotor Failure Conditions
title_sort adaptive observer-based fault detection and fault-tolerant control of quadrotors under rotor failure conditions
publisher MDPI AG
series Applied Sciences
issn 2076-3417
publishDate 2020-05-01
description This paper aims to propose a strategy for the flight control of quad-rotors under single rotor failure conditions. The proposed control strategy consists of two stages—fault detection (FD) and fault tolerant control (FTC). A dual observer-based strategy for FD and fault estimation is developed. With the combination of the results from both observers, the decision making in whether a fault actually happened or the observed anomaly was caused by an external disturbance could be distinguished. Following the FD result, a control strategy for normal flight, as well as the abnormal one, is presented. The FTC considers a real-time coordinate transformation scheme to manipulate the target angles for the quad-rotor to follow a prescribed trajectory. When a rotor fault happens, it is going to be detected by the dual observers and then the FTC is activated to stabilize the system such that the trajectory following task can still be fulfilled. Furthermore, in order to achieve robust flight in the presence of external wind perturbation, the sliding mode control (SMC) theory is further integrated. Simulations illustrate the effectiveness and feasibility of the proposed method.
topic quadrotor
actuator fault
fault detection
fault tolerant control
sliding mode control
url https://www.mdpi.com/2076-3417/10/10/3503
work_keys_str_mv AT yuhsuanlien adaptiveobserverbasedfaultdetectionandfaulttolerantcontrolofquadrotorsunderrotorfailureconditions
AT chaochungpeng adaptiveobserverbasedfaultdetectionandfaulttolerantcontrolofquadrotorsunderrotorfailureconditions
AT yihsuanchen adaptiveobserverbasedfaultdetectionandfaulttolerantcontrolofquadrotorsunderrotorfailureconditions
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