Trajectory control approaches for a fault tolerant quadcopter

Alexandre Brito; Vasco Brito; Luís Brito Palma; Fernando Coito; Paulo Gil

doi:10.1109/YEF-ECE.2018.8368932

Trajectory control approaches for a fault tolerant quadcopter

Alexandre Brito, Vasco Brito, Luís Brito Palma, Fernando Coito, Paulo Gil

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

2 Citations (Scopus)

Abstract

This article is focused in exploring the most efficient forms of flying towards its destination through predetermined waypoints, with the presented fault tolerant X8 architecture, considering its energy consumption and total flight time. This paper's content will go through the quadcopter kinematic and dynamic model, the extension to the X8 model and the comparison of the PID, State Feedback control and Differential Flatness algorithms developed for the quadcopter X8 maneuvering. Faults/failures in actuators are also considered and studied.

Original language	English
Title of host publication	Proceedings - 2018 International Young Engineers Forum, YEF-ECE 2018
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	13-18
Number of pages	6
ISBN (Electronic)	9781538615034
DOIs	https://doi.org/10.1109/YEF-ECE.2018.8368932
Publication status	Published - 29 May 2018
Event	2nd International Young Engineers Forum, YEF-ECE 2018 - Caparica, Portugal Duration: 4 May 2018 → 4 May 2018

Conference

Conference	2nd International Young Engineers Forum, YEF-ECE 2018
Country/Territory	Portugal
City	Caparica
Period	4/05/18 → 4/05/18

Keywords

Fault Tolerant Control
Faults and Failures
Quadcopter
Trajectory Control

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Access to Document

10.1109/YEF-ECE.2018.8368932

Cite this

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title = "Trajectory control approaches for a fault tolerant quadcopter",

abstract = "This article is focused in exploring the most efficient forms of flying towards its destination through predetermined waypoints, with the presented fault tolerant X8 architecture, considering its energy consumption and total flight time. This paper's content will go through the quadcopter kinematic and dynamic model, the extension to the X8 model and the comparison of the PID, State Feedback control and Differential Flatness algorithms developed for the quadcopter X8 maneuvering. Faults/failures in actuators are also considered and studied.",

keywords = "Fault Tolerant Control, Faults and Failures, Quadcopter, Trajectory Control",

author = "Alexandre Brito and Vasco Brito and Palma, {Lu{\'i}s Brito} and Fernando Coito and Paulo Gil",

note = "info:eu-repo/grantAgreement/FCT/5876/147324/PT# ; 2nd International Young Engineers Forum, YEF-ECE 2018 ; Conference date: 04-05-2018 Through 04-05-2018",

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doi = "10.1109/YEF-ECE.2018.8368932",

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Brito, A , Brito, V , Palma, LB , Coito, F & Gil, P 2018, Trajectory control approaches for a fault tolerant quadcopter. in Proceedings - 2018 International Young Engineers Forum, YEF-ECE 2018. Institute of Electrical and Electronics Engineers Inc., pp. 13-18, 2nd International Young Engineers Forum, YEF-ECE 2018, Caparica, Portugal, 4/05/18. https://doi.org/10.1109/YEF-ECE.2018.8368932

TY - GEN

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AU - Brito, Alexandre

AU - Brito, Vasco

AU - Palma, Luís Brito

AU - Coito, Fernando

AU - Gil, Paulo

N1 - info:eu-repo/grantAgreement/FCT/5876/147324/PT#

PY - 2018/5/29

Y1 - 2018/5/29

N2 - This article is focused in exploring the most efficient forms of flying towards its destination through predetermined waypoints, with the presented fault tolerant X8 architecture, considering its energy consumption and total flight time. This paper's content will go through the quadcopter kinematic and dynamic model, the extension to the X8 model and the comparison of the PID, State Feedback control and Differential Flatness algorithms developed for the quadcopter X8 maneuvering. Faults/failures in actuators are also considered and studied.

AB - This article is focused in exploring the most efficient forms of flying towards its destination through predetermined waypoints, with the presented fault tolerant X8 architecture, considering its energy consumption and total flight time. This paper's content will go through the quadcopter kinematic and dynamic model, the extension to the X8 model and the comparison of the PID, State Feedback control and Differential Flatness algorithms developed for the quadcopter X8 maneuvering. Faults/failures in actuators are also considered and studied.

KW - Fault Tolerant Control

KW - Faults and Failures

KW - Quadcopter

KW - Trajectory Control

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M3 - Conference contribution

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BT - Proceedings - 2018 International Young Engineers Forum, YEF-ECE 2018

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2nd International Young Engineers Forum, YEF-ECE 2018

Y2 - 4 May 2018 through 4 May 2018

ER -

Trajectory control approaches for a fault tolerant quadcopter

Abstract

Conference

Keywords

UN SDGs

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