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25099

THE EFFECT OF THE EARTH'S OBLATENESS AND ATMOSPHERIC DRAG ON AN ARTIFICIAL SATELLITE IN TERMS OF THE EULER PARAMETERS

Article

Last updated: 04 Jan 2025

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Abstract

This paper is concerned with an orbit prediction using the Euler variables. Perturbations due to the Earth's gravitational field up to the fourth zonal harmonic and the atmospheric drag with rotating & non-rotating atmosphere are considered. The method developed is illustrated by application to a typical satellite orbit. A final state of accuracy 10.3 m is obtained.

DOI

10.21608/asat.1999.25099

Keywords

Artificial satellite, Earth's oblateness, atmospheric drag, Euler parameters

Authors

First Name

M.

Last Name

AWAD

MiddleName

E.

Affiliation

Department of Astronomy, Cairo University, Egypt.

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City

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Orcid

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First Name

M.

Last Name

AHMED

MiddleName

K.

Affiliation

Department of Astronomy, Cairo University, Egypt.

Email

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City

-

Orcid

-

First Name

M.

Last Name

EL-SHAARAY

MiddleName

B.

Affiliation

Department of Astronomy, AL-Azhar University, Egypt.

Email

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City

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Orcid

-

First Name

I.

Last Name

HASSAN

MiddleName

A.

Affiliation

Department of Astronomy, AL-Azhar University, Egypt.

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-

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Orcid

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Volume

8

Article Issue

ASAT Conference, 4-6 May 1999

Related Issue

4551

Issue Date

1999-05-01

Receive Date

2019-01-17

Publish Date

1999-05-01

Page Start

1

Page End

24

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 8_Issue ASAT Conference, 4-6 May 1999_Pages 1-24.pdf

PDF . 2.3MB

Link

https://asat.journals.ekb.eg/article_25099.html

Detail API

https://asat.journals.ekb.eg/service?article_code=25099

Order

45

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

THE EFFECT OF THE EARTH'S OBLATENESS AND ATMOSPHERIC DRAG ON AN ARTIFICIAL SATELLITE IN TERMS OF THE EULER PARAMETERS

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Article

Created At

22 Jan 2023