Dynamic model of an aircraft propulsion system with electric motor and propeller

Manuela Montoya Rivera; Luis Benigno Gutierrez

doi:10.1109/CCAC51819.2021.9633324

Dynamic model of an aircraft propulsion system with electric motor and propeller

Manuela Montoya Rivera
, Luis Benigno Gutierrez

Producción científica: Capítulo de libro/acta de congreso con ISBN › Ponencia publicada en las memorias del evento con ISBN › revisión exhaustiva

1 Cita (Scopus)

Resumen

This paper presents a mathematical model for the dynamic behavior of a electric propulsion system for an aircraft. The system is composed of a Li-Po battery, an electronic speed control (ESC), a brushless DC motor (BLDC), and a propeller. Models are obtained for each component of the system and then they are implemented and integrated for numerical simulation in m language in Octave. The model takes into account the hybrid nature of the system, given that the switching dynamics of the ESC is considered as a discrete event model, while the dynamics of the other components is continuous. The parameters used in the simulation have realistic values associated to the model of a small unmanned aerial vehicle (UAV) propulsion system, but with adecuate parameters it could represent the dynamics of a larger scale electric manned aircraft. Simulation results show a reasonable behavior and further work will be done to estimate the parameters for a real UAV prototype, based on the proposed model.

Idioma original	Inglés
Título de la publicación alojada	Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021
Editores	Diana Marcela Ovalle Martinez, Luis Francisco Combita Alfonso
Editorial	Institute of Electrical and Electronics Engineers Inc.
Páginas	157-162
Número de páginas	6
ISBN (versión digital)	9781665418836
DOI	https://doi.org/10.1109/CCAC51819.2021.9633324
Estado	Publicada - 2021
Evento	5th IEEE Colombian Conference on Automatic Control, CCAC 2021 - Ibague, Colombia Duración: 19 oct. 2021 → 22 oct. 2021

Serie de la publicación

Nombre	Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021

Conferencia

Conferencia	5th IEEE Colombian Conference on Automatic Control, CCAC 2021
País/Territorio	Colombia
Ciudad	Ibague
Período	19/10/21 → 22/10/21

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© 2021 IEEE.

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10.1109/CCAC51819.2021.9633324

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Rivera, M. M., & Gutierrez, L. B. (2021). Dynamic model of an aircraft propulsion system with electric motor and propeller. En D. M. O. Martinez, & L. F. C. Alfonso (Eds.), Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021 (pp. 157-162). (Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/CCAC51819.2021.9633324

Rivera, Manuela Montoya ; Gutierrez, Luis Benigno. / Dynamic model of an aircraft propulsion system with electric motor and propeller. Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021. editor / Diana Marcela Ovalle Martinez ; Luis Francisco Combita Alfonso. Institute of Electrical and Electronics Engineers Inc., 2021. pp. 157-162 (Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021).

@inproceedings{2385317393e449d48fba1d5ab349d783,

title = "Dynamic model of an aircraft propulsion system with electric motor and propeller",

abstract = "This paper presents a mathematical model for the dynamic behavior of a electric propulsion system for an aircraft. The system is composed of a Li-Po battery, an electronic speed control (ESC), a brushless DC motor (BLDC), and a propeller. Models are obtained for each component of the system and then they are implemented and integrated for numerical simulation in m language in Octave. The model takes into account the hybrid nature of the system, given that the switching dynamics of the ESC is considered as a discrete event model, while the dynamics of the other components is continuous. The parameters used in the simulation have realistic values associated to the model of a small unmanned aerial vehicle (UAV) propulsion system, but with adecuate parameters it could represent the dynamics of a larger scale electric manned aircraft. Simulation results show a reasonable behavior and further work will be done to estimate the parameters for a real UAV prototype, based on the proposed model.",

keywords = "Aircraft electrical propulsion, Dynamic model, Electric motor, Electronic Speed Control, Li-Po battery, Octave, Propeller",

author = "Rivera, \{Manuela Montoya\} and Gutierrez, \{Luis Benigno\}",

note = "Publisher Copyright: {\textcopyright} 2021 IEEE.; 5th IEEE Colombian Conference on Automatic Control, CCAC 2021 ; Conference date: 19-10-2021 Through 22-10-2021",

year = "2021",

doi = "10.1109/CCAC51819.2021.9633324",

language = "Ingl{\'e}s",

series = "Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

pages = "157--162",

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booktitle = "Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021",

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Rivera, MM & Gutierrez, LB 2021, Dynamic model of an aircraft propulsion system with electric motor and propeller. En DMO Martinez & LFC Alfonso (eds.), Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021. Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021, Institute of Electrical and Electronics Engineers Inc., pp. 157-162, 5th IEEE Colombian Conference on Automatic Control, CCAC 2021, Ibague, Colombia, 19/10/21. https://doi.org/10.1109/CCAC51819.2021.9633324

Dynamic model of an aircraft propulsion system with electric motor and propeller. / Rivera, Manuela Montoya; Gutierrez, Luis Benigno.
Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021. ed. / Diana Marcela Ovalle Martinez; Luis Francisco Combita Alfonso. Institute of Electrical and Electronics Engineers Inc., 2021. p. 157-162 (Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021).

Producción científica: Capítulo de libro/acta de congreso con ISBN › Ponencia publicada en las memorias del evento con ISBN › revisión exhaustiva

TY - GEN

T1 - Dynamic model of an aircraft propulsion system with electric motor and propeller

AU - Rivera, Manuela Montoya

AU - Gutierrez, Luis Benigno

PY - 2021

Y1 - 2021

N2 - This paper presents a mathematical model for the dynamic behavior of a electric propulsion system for an aircraft. The system is composed of a Li-Po battery, an electronic speed control (ESC), a brushless DC motor (BLDC), and a propeller. Models are obtained for each component of the system and then they are implemented and integrated for numerical simulation in m language in Octave. The model takes into account the hybrid nature of the system, given that the switching dynamics of the ESC is considered as a discrete event model, while the dynamics of the other components is continuous. The parameters used in the simulation have realistic values associated to the model of a small unmanned aerial vehicle (UAV) propulsion system, but with adecuate parameters it could represent the dynamics of a larger scale electric manned aircraft. Simulation results show a reasonable behavior and further work will be done to estimate the parameters for a real UAV prototype, based on the proposed model.

AB - This paper presents a mathematical model for the dynamic behavior of a electric propulsion system for an aircraft. The system is composed of a Li-Po battery, an electronic speed control (ESC), a brushless DC motor (BLDC), and a propeller. Models are obtained for each component of the system and then they are implemented and integrated for numerical simulation in m language in Octave. The model takes into account the hybrid nature of the system, given that the switching dynamics of the ESC is considered as a discrete event model, while the dynamics of the other components is continuous. The parameters used in the simulation have realistic values associated to the model of a small unmanned aerial vehicle (UAV) propulsion system, but with adecuate parameters it could represent the dynamics of a larger scale electric manned aircraft. Simulation results show a reasonable behavior and further work will be done to estimate the parameters for a real UAV prototype, based on the proposed model.

KW - Aircraft electrical propulsion

KW - Dynamic model

KW - Electric motor

KW - Electronic Speed Control

KW - Li-Po battery

KW - Octave

KW - Propeller

UR - https://www.scopus.com/pages/publications/85124163243

U2 - 10.1109/CCAC51819.2021.9633324

DO - 10.1109/CCAC51819.2021.9633324

M3 - Ponencia publicada en las memorias del evento con ISBN

AN - SCOPUS:85124163243

T3 - Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021

SP - 157

EP - 162

BT - Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021

A2 - Martinez, Diana Marcela Ovalle

A2 - Alfonso, Luis Francisco Combita

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 5th IEEE Colombian Conference on Automatic Control, CCAC 2021

Y2 - 19 October 2021 through 22 October 2021

ER -

Rivera MM, Gutierrez LB. Dynamic model of an aircraft propulsion system with electric motor and propeller. En Martinez DMO, Alfonso LFC, editores, Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021. Institute of Electrical and Electronics Engineers Inc. 2021. p. 157-162. (Proceedings of the 2021 IEEE 5th Colombian Conference on Automatic Control, CCAC 2021). doi: 10.1109/CCAC51819.2021.9633324

Dynamic model of an aircraft propulsion system with electric motor and propeller

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