Experimental Investigation for RUAV's Actuator Fault Detections with AESMF

The adaptive extended set-membership filter (AESMF) algorithm for robots' online modelling is today proposed for use in this field. Compared to the traditional ESMF, this novel filter method improves estimation accuracy under variable boundaries of unknown but bounded (UBB) process noise, which...

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Main Authors: Dalei Song, Juntong Qi, Liying Yang, Jianda Han
Format: Article
Language:English
Published: SAGE Publishing 2015-07-01
Series:International Journal of Advanced Robotic Systems
Online Access:https://doi.org/10.5772/60854
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spelling doaj-dcabea166b5d4edab339a631f4512aa92020-11-25T03:02:54ZengSAGE PublishingInternational Journal of Advanced Robotic Systems1729-88142015-07-011210.5772/6085410.5772_60854Experimental Investigation for RUAV's Actuator Fault Detections with AESMFDalei Song0Juntong Qi1Liying Yang2Jianda Han3The State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang, ChinaThe State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang, ChinaThe State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang, ChinaThe State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang, ChinaThe adaptive extended set-membership filter (AESMF) algorithm for robots' online modelling is today proposed for use in this field. Compared to the traditional ESMF, this novel filter method improves estimation accuracy under variable boundaries of unknown but bounded (UBB) process noise, which is often caused by the uncertainties of robotic dynamics. However, the applicability and stability of the AESMF method have not been tested in detail or demonstrated for real robotic systems. In this research, AESMF is applied for the actuator fault detections of a rotor-craft unmanned air vehicle (RUAV). The stability of AESMF is firstly analysed using mathematics and actuator healthy coefficients (AHC) are introduced for building the actuator failure model of RUAVs. AESMF is employed for the online boundary estimation of flight states and AHC parameters for fault tolerance control. Based on the proposed AESMF actuator fault estimation, flight experiments are conducted using a ServoHeli-40 RUAV platform and the flight results are compared with traditional ESMF and the adaptive extended Kalman filter (AEKF) in order to demonstrate its effectiveness, as well as for suggesting improvements for the actuator failure detection of RUAVs.https://doi.org/10.5772/60854
collection DOAJ
language English
format Article
sources DOAJ
author Dalei Song
Juntong Qi
Liying Yang
Jianda Han
spellingShingle Dalei Song
Juntong Qi
Liying Yang
Jianda Han
Experimental Investigation for RUAV's Actuator Fault Detections with AESMF
International Journal of Advanced Robotic Systems
author_facet Dalei Song
Juntong Qi
Liying Yang
Jianda Han
author_sort Dalei Song
title Experimental Investigation for RUAV's Actuator Fault Detections with AESMF
title_short Experimental Investigation for RUAV's Actuator Fault Detections with AESMF
title_full Experimental Investigation for RUAV's Actuator Fault Detections with AESMF
title_fullStr Experimental Investigation for RUAV's Actuator Fault Detections with AESMF
title_full_unstemmed Experimental Investigation for RUAV's Actuator Fault Detections with AESMF
title_sort experimental investigation for ruav's actuator fault detections with aesmf
publisher SAGE Publishing
series International Journal of Advanced Robotic Systems
issn 1729-8814
publishDate 2015-07-01
description The adaptive extended set-membership filter (AESMF) algorithm for robots' online modelling is today proposed for use in this field. Compared to the traditional ESMF, this novel filter method improves estimation accuracy under variable boundaries of unknown but bounded (UBB) process noise, which is often caused by the uncertainties of robotic dynamics. However, the applicability and stability of the AESMF method have not been tested in detail or demonstrated for real robotic systems. In this research, AESMF is applied for the actuator fault detections of a rotor-craft unmanned air vehicle (RUAV). The stability of AESMF is firstly analysed using mathematics and actuator healthy coefficients (AHC) are introduced for building the actuator failure model of RUAVs. AESMF is employed for the online boundary estimation of flight states and AHC parameters for fault tolerance control. Based on the proposed AESMF actuator fault estimation, flight experiments are conducted using a ServoHeli-40 RUAV platform and the flight results are compared with traditional ESMF and the adaptive extended Kalman filter (AEKF) in order to demonstrate its effectiveness, as well as for suggesting improvements for the actuator failure detection of RUAVs.
url https://doi.org/10.5772/60854
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AT juntongqi experimentalinvestigationforruavsactuatorfaultdetectionswithaesmf
AT liyingyang experimentalinvestigationforruavsactuatorfaultdetectionswithaesmf
AT jiandahan experimentalinvestigationforruavsactuatorfaultdetectionswithaesmf
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