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23480

Evolution of the Motion Around a Slowly Rotating Body

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Last updated: 04 Jan 2025

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Abstract

The motion of a satellite about a rotating triaxial body will be investigated, stressing on the case of slow rotation. The Hamiltonian of the problem will be formed including the zonal harmonic J2 and the leading tesseral harmonics C22 and S22. The small parameter of the problem is the spin rate (σ) of the primary. The solution proceeds through three canonical transformations to eliminate in succession; the short, intermediate and longperiod terms. Thus secular and periodic terms are to be retained up to orders four and two respectively.

DOI

10.21608/asat.2009.23480

Authors

First Name

W.

Last Name

El-Mahy

MiddleName

M.

Affiliation

Cairo University.

Email

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City

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Orcid

-

First Name

M.

Last Name

Ahmed

MiddleName

K.

Affiliation

Cairo University.

Email

-

City

-

Orcid

-

First Name

M.

Last Name

Awad

MiddleName

A.

Affiliation

Cairo University.

Email

-

City

-

Orcid

-

First Name

Z.

Last Name

Hayman

MiddleName

M.

Affiliation

Cairo University.

Email

-

City

-

Orcid

-

Volume

13

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT- 13, May 26 – 28, 2009

Related Issue

4377

Issue Date

2009-05-01

Receive Date

2019-01-03

Publish Date

2009-05-01

Page Start

1

Page End

10

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_23480.html

Detail API

https://asat.journals.ekb.eg/service?article_code=23480

Order

11

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

Evolution of the Motion Around a Slowly Rotating Body

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Article

Created At

22 Jan 2023