Passive Fault Tolerant Lateral Controller Design For an UAV

Sıtkı Yenal Vural; Janset Dasdemir; Chingiz Hajiyev

doi:10.1016/j.ifacol.2018.11.320

Passive Fault Tolerant Lateral Controller Design For an UAV

Sıtkı Yenal Vural, Janset Dasdemir, Chingiz Hajiyev

Department of Aeronautical Engineering

Research output: Contribution to journal › Article › peer-review

11 Citations (Scopus)

Abstract

In this study a passive lateral fault tolerant controller for an UAV is designed using dynamic inversion (DI) method and robust integral of the signum of the error (RISE) techniques. The details of the methods are summarized. As the reference model of the tracking controller, UAV controlled by feedback type controller is used and the control method used for this design is explained. The loss in control effectiveness is modeled as changes in the control distribution matrix. Simulations are made to show the effectiveness of the passive fault tolerant controller in maintaining the lateral control in case of actuator effectiveness loss.

Original language	English
Pages (from-to)	446-451
Number of pages	6
Journal	IFAC-PapersOnLine
Volume	51
Issue number	30
DOIs	https://doi.org/10.1016/j.ifacol.2018.11.320
Publication status	Published - 2018

Bibliographical note

Publisher Copyright:
© 2016

Keywords

Actuator failure
Fault-tolerant control
Robust control
UAV control
UAVs

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10.1016/j.ifacol.2018.11.320

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abstract = "In this study a passive lateral fault tolerant controller for an UAV is designed using dynamic inversion (DI) method and robust integral of the signum of the error (RISE) techniques. The details of the methods are summarized. As the reference model of the tracking controller, UAV controlled by feedback type controller is used and the control method used for this design is explained. The loss in control effectiveness is modeled as changes in the control distribution matrix. Simulations are made to show the effectiveness of the passive fault tolerant controller in maintaining the lateral control in case of actuator effectiveness loss.",

keywords = "Actuator failure, Fault-tolerant control, Robust control, UAV control, UAVs",

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AU - Dasdemir, Janset

AU - Hajiyev, Chingiz

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AB - In this study a passive lateral fault tolerant controller for an UAV is designed using dynamic inversion (DI) method and robust integral of the signum of the error (RISE) techniques. The details of the methods are summarized. As the reference model of the tracking controller, UAV controlled by feedback type controller is used and the control method used for this design is explained. The loss in control effectiveness is modeled as changes in the control distribution matrix. Simulations are made to show the effectiveness of the passive fault tolerant controller in maintaining the lateral control in case of actuator effectiveness loss.

KW - Actuator failure

KW - Fault-tolerant control

KW - Robust control

KW - UAV control

KW - UAVs

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JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

IS - 30

ER -

Passive Fault Tolerant Lateral Controller Design For an UAV

Abstract

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Keywords

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