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Detection time analysis of propulsion system fault effects in a hexacopter

Research output: Contributions to collected editions/works › Article in conference proceedings › Research › peer-review

Standard

Detection time analysis of propulsion system fault effects in a hexacopter. / Santos, M. F.; Honorio, L. M.; Costa, E. B. et al.
Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019. ed. / Andrzej Kot; Agata Nawrocka. IEEE - Institute of Electrical and Electronics Engineers Inc., 2019. 8765990 (Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019).

Research output: Contributions to collected editions/works › Article in conference proceedings › Research › peer-review

Harvard

Santos, MF, Honorio, LM, Costa, EB, Silva, MF, Vidal, VF, Santos Neto, AF, Rezende, HB, Mercorelli, P & Pancoti, AAN 2019, Detection time analysis of propulsion system fault effects in a hexacopter. in A Kot & A Nawrocka (eds), Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019., 8765990, Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019, IEEE - Institute of Electrical and Electronics Engineers Inc., 20st International Carpathian Control Conference - ICCC 2019, Kraków - Wieliczka, Poland, 26.05.19. https://doi.org/10.1109/CarpathianCC.2019.8765990

APA

Santos, M. F., Honorio, L. M., Costa, E. B., Silva, M. F., Vidal, V. F., Santos Neto, A. F., Rezende, H. B., Mercorelli, P., & Pancoti, A. A. N. (2019). Detection time analysis of propulsion system fault effects in a hexacopter. In A. Kot, & A. Nawrocka (Eds.), Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019 Article 8765990 (Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019). IEEE - Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CarpathianCC.2019.8765990

Vancouver

Santos MF, Honorio LM, Costa EB, Silva MF, Vidal VF, Santos Neto AF et al. Detection time analysis of propulsion system fault effects in a hexacopter. In Kot A, Nawrocka A, editors, Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019. IEEE - Institute of Electrical and Electronics Engineers Inc. 2019. 8765990. (Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019). doi: 10.1109/CarpathianCC.2019.8765990

Bibtex

@inbook{f4627a82baf94dad8eb49caec944cf58,
title = "Detection time analysis of propulsion system fault effects in a hexacopter",
abstract = "The hexacopter propulsion system is composed of electronic speed controllers, motors and propellers. When severe damage happens in one of these components, critical impacts over the system's dynamics are witnessed. Changing the controller parameters or even adopting a different control strategy is useless once the system loses its controllability. To prevent significant damages, this work presents a case study about the detection time effects that total faults interfere with the aircraft dynamics, which is extremely necessary to be identified and perceived by the aircraft control board. The case study was built using nonintrusive indices, based on an error from angular dynamics responses. Once identified a failure situation, a future control device can provide some performance actions due to critical issues, without losing the aircraft controllability or leaving it to crash. The results were impressive, showing that it is possible to develop fault detection and identification technique in 0.1 seconds tops, keeping the aircraft safe in these scenarios. Longer detection time may lead to insert non-controllable cases.",
keywords = "Engineering, Fault Detection Time Analysis, Hexacopter, Non-Intrusive Indices, Fault Detection Time Analysis, Hexacopter, Non-Intrusive Indices",
author = "Santos, {M. F.} and Honorio, {L. M.} and Costa, {E. B.} and Silva, {M. F.} and Vidal, {V. F.} and {Santos Neto}, {A. F.} and Rezende, {H. B.} and P. Mercorelli and Pancoti, {A. A.N.}",
note = "Funding Information: ACKNOWLEDGMENT The authors would like to thank CEFET-MG, UFJF and Leuphana University of Lneburg for the financial support. Publisher Copyright: {\textcopyright} 2019 IEEE.; 20st International Carpathian Control Conference - ICCC 2019, ICCC ; Conference date: 26-05-2019 Through 29-05-2019",
year = "2019",
month = may,
day = "1",
doi = "10.1109/CarpathianCC.2019.8765990",
language = "English",
series = "Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019",
publisher = "IEEE - Institute of Electrical and Electronics Engineers Inc.",
editor = "Andrzej Kot and Agata Nawrocka",
booktitle = "Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019",
address = "United States",
url = "https://iccc.agh.edu.pl/",

}

RIS

TY - CHAP

T1 - Detection time analysis of propulsion system fault effects in a hexacopter

AU - Santos, M. F.

AU - Honorio, L. M.

AU - Costa, E. B.

AU - Silva, M. F.

AU - Vidal, V. F.

AU - Santos Neto, A. F.

AU - Rezende, H. B.

AU - Mercorelli, P.

AU - Pancoti, A. A.N.

N1 - Conference code: 20

PY - 2019/5/1

Y1 - 2019/5/1

N2 - The hexacopter propulsion system is composed of electronic speed controllers, motors and propellers. When severe damage happens in one of these components, critical impacts over the system's dynamics are witnessed. Changing the controller parameters or even adopting a different control strategy is useless once the system loses its controllability. To prevent significant damages, this work presents a case study about the detection time effects that total faults interfere with the aircraft dynamics, which is extremely necessary to be identified and perceived by the aircraft control board. The case study was built using nonintrusive indices, based on an error from angular dynamics responses. Once identified a failure situation, a future control device can provide some performance actions due to critical issues, without losing the aircraft controllability or leaving it to crash. The results were impressive, showing that it is possible to develop fault detection and identification technique in 0.1 seconds tops, keeping the aircraft safe in these scenarios. Longer detection time may lead to insert non-controllable cases.

AB - The hexacopter propulsion system is composed of electronic speed controllers, motors and propellers. When severe damage happens in one of these components, critical impacts over the system's dynamics are witnessed. Changing the controller parameters or even adopting a different control strategy is useless once the system loses its controllability. To prevent significant damages, this work presents a case study about the detection time effects that total faults interfere with the aircraft dynamics, which is extremely necessary to be identified and perceived by the aircraft control board. The case study was built using nonintrusive indices, based on an error from angular dynamics responses. Once identified a failure situation, a future control device can provide some performance actions due to critical issues, without losing the aircraft controllability or leaving it to crash. The results were impressive, showing that it is possible to develop fault detection and identification technique in 0.1 seconds tops, keeping the aircraft safe in these scenarios. Longer detection time may lead to insert non-controllable cases.

KW - Engineering

KW - Fault Detection Time Analysis

KW - Hexacopter

KW - Non-Intrusive Indices

KW - Fault Detection Time Analysis

KW - Hexacopter

KW - Non-Intrusive Indices

UR - http://www.scopus.com/inward/record.url?scp=85069831452&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/0e5cd4c4-efd1-3836-af82-7f8acf67adaf/

U2 - 10.1109/CarpathianCC.2019.8765990

DO - 10.1109/CarpathianCC.2019.8765990

M3 - Article in conference proceedings

T3 - Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019

BT - Proceedings of the 2019 20th International Carpathian Control Conference, ICCC 2019

A2 - Kot, Andrzej

A2 - Nawrocka, Agata

PB - IEEE - Institute of Electrical and Electronics Engineers Inc.

T2 - 20st International Carpathian Control Conference - ICCC 2019

Y2 - 26 May 2019 through 29 May 2019

ER -

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Advancing Sustainability and Productivity: The Role of Precision Agriculture in Vineyards and Olive Groves

Fernandes, F. M., Dos Santos, M. F., De Morais, M. H. F., Lima, J., Pereira, A. I. & Mercorelli, P., 2025, Proceedings of the 2025 26th International Carpathian Control Conference (ICCC): Grandhotel Starý Smokovec, High Tatras, Starý Smokovec, Slovak Republic, 19-21 May 2025. Kacur, J., Skovranek, T., Laciak, M. & Mojzisova, A. (eds.). Piscataway: Institute of Electrical and Electronics Engineers Inc., 6 p. (International Carpathian Control Conference, ICCC; vol. 26).

Research output: Contributions to collected editions/works › Article in conference proceedings › Research › peer-review

A Fluid Elastomeric Actuator Design for Soft Robots

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Research output: Journal contributions › Journal articles › Research › peer-review

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Li, X., Zhang, Q., Gu, H., Othmen, S., Asklany, S., Lhioui, C., Elrashidi, A. & Mercorelli, P., 07.2025, In: PLoS ONE. 20, 7, 22 p., e0327249.

Research output: Journal contributions › Journal articles › Research › peer-review

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Pimentel, G. O., Santos, M. F. D., Lima, J., Mercorelli, P. & Fernandes, F. M., 15.01.2025, In: Sensors. 25, 2, 27 p., 479.

Research output: Journal contributions › Journal articles › Research › peer-review

Automatic Tuning of Extended Kalman Filter in Synchronous Reluctance Motor Drives with a Master-Slave Configuration

Rigon, S., Haus, B., Mercorelli, P. & Zigliotto, M., 27.02.2025, In: IEEE Open Journal of Power Electronics. 6, p. 734-746 13 p.

Research output: Journal contributions › Journal articles › Research › peer-review

DOI

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