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22456

Micro Air Vehicle Nonlinear Simulation

Article

Last updated: 04 Jan 2025

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Abstract

Micro air vehicle (MAV) is very sensitive to the external disturbances which make the prediction of its dynamics a hard task. In this paper there is a description of nonlinear simulation made for the MAV's dynamics prediction. Experimental measured data were used in this Simulink simulation, the Aerodynamics forces and moment, Mass moment of inertia, and propulsion system performance were experimentally measured for an accurate simulation of the MAV. The output from the simulation gave accurate prediction for the MAV dynamics.

DOI

10.21608/asat.2017.22456

Keywords

nonlinear, SIMULINK, MAV, flight dynamics

Authors

First Name

Ahmed

Last Name

AboElezz

MiddleName

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Affiliation

Aerodynamics laboratory engineer, IAET.

Email

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City

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Orcid

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First Name

Ahmed

Last Name

Desoki

MiddleName

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Affiliation

Assistant professor, Aerospace department, Cairo university.

Email

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City

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Orcid

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First Name

Basman

Last Name

Elhadidi

MiddleName

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Affiliation

Professor Aerospace department, Cairo university.

Email

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City

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Orcid

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First Name

Gamal

Last Name

El-Bayoumi

MiddleName

-

Affiliation

Professor Aerospace department, Cairo university.

Email

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City

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Orcid

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Volume

17

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 – April 11 - 13, 2017

Related Issue

4266

Issue Date

2017-04-01

Receive Date

2018-12-20

Publish Date

2017-04-01

Page Start

1

Page End

13

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 17_Issue AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 &nd….pdf

PDF . 1.1MB

Link

https://asat.journals.ekb.eg/article_22456.html

Detail API

https://asat.journals.ekb.eg/service?article_code=22456

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Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Micro Air Vehicle Nonlinear Simulation

Details

Type

Article

Created At

22 Jan 2023