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Fixed-Time Observer Based Safety Control for a Quadrotor UAV
This article presents a fixed-time observer-based safety control strategy for quadrotor unmanned aerial vehicles (UAVs) against multiple actuator faults and unknown disturbances. The fixed-time sliding mode observer is designed to estimate the state residual and the unknown actuator fault. Unlike mo...
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Published in: | IEEE transactions on aerospace and electronic systems 2021-10, Vol.57 (5), p.2815-2825 |
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container_title | IEEE transactions on aerospace and electronic systems |
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creator | Zhou, Sicheng Guo, Kexin Yu, Xiang Guo, Lei Xie, Lihua |
description | This article presents a fixed-time observer-based safety control strategy for quadrotor unmanned aerial vehicles (UAVs) against multiple actuator faults and unknown disturbances. The fixed-time sliding mode observer is designed to estimate the state residual and the unknown actuator fault. Unlike most of the existing safety control strategies, the estimation time of the fault parameters is independent of initial condition, which can be strictly ensured within a fixed upper bound. Besides, the transient estimation error is regarded as a disturbance. In this article, a retrofit control mechanism with integration of the fixed-time estimator and an integral sliding mode controller is devised against multiple actuator faults and disturbances. Finally, both simulation and experimental tests demonstrate the effectiveness of the proposed UAV safety control. |
doi_str_mv | 10.1109/TAES.2021.3068434 |
format | article |
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The fixed-time sliding mode observer is designed to estimate the state residual and the unknown actuator fault. Unlike most of the existing safety control strategies, the estimation time of the fault parameters is independent of initial condition, which can be strictly ensured within a fixed upper bound. Besides, the transient estimation error is regarded as a disturbance. In this article, a retrofit control mechanism with integration of the fixed-time estimator and an integral sliding mode controller is devised against multiple actuator faults and disturbances. 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Finally, both simulation and experimental tests demonstrate the effectiveness of the proposed UAV safety control.</description><subject>Actuator faults</subject><subject>Actuators</subject><subject>Brushless motors</subject><subject>Disturbances</subject><subject>Estimation error</subject><subject>fixed-time observer</subject><subject>Observers</subject><subject>quadrotor unmanned aerial vehicle (UAV)</subject><subject>Retrofitting</subject><subject>Safety</subject><subject>safety control</subject><subject>Sliding mode control</subject><subject>Transient analysis</subject><subject>transient estimation error</subject><subject>Unmanned aerial vehicles</subject><subject>Unmanned helicopters</subject><subject>Upper bounds</subject><issn>0018-9251</issn><issn>1557-9603</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNo9kE1rAjEQhkNpodb2B5ReFnpeO_lOoBcr2hYEKWqvIZvNwooam6xF_30jSk8zA887MzwIPWIYYAz6ZTEczwcECB5QEIpRdoV6mHNZagH0GvUAsCo14fgW3aW0yiPLVA-9TtqDr8tFu_HFrEo-_vpYvNnk62JuG98di1HYdjGsiybEwhZfe1vH0OV-Ofy-RzeNXSf_cKl9tJyMF6OPcjp7_xwNp6UjmnYlpoTZytZcMiwdqEooIYVrVE055J8UqYTDVFnHFEiHgXOnOZNE2VoLQmkfPZ_37mL42fvUmVXYx20-aXIaQGuuIVP4TLkYUoq-MbvYbmw8GgzmJMmcJJmTJHORlDNP50zrvf_nNVVcaUn_AMzVX6o</recordid><startdate>20211001</startdate><enddate>20211001</enddate><creator>Zhou, Sicheng</creator><creator>Guo, Kexin</creator><creator>Yu, Xiang</creator><creator>Guo, Lei</creator><creator>Xie, Lihua</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. 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subjects | Actuator faults Actuators Brushless motors Disturbances Estimation error fixed-time observer Observers quadrotor unmanned aerial vehicle (UAV) Retrofitting Safety safety control Sliding mode control Transient analysis transient estimation error Unmanned aerial vehicles Unmanned helicopters Upper bounds |
title | Fixed-Time Observer Based Safety Control for a Quadrotor UAV |
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