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34732

HIGH ACCURACY SPACECRAFT ORBIT PROPAGATOR VALIDATION

Article

Last updated: 04 Jan 2025

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Abstract

ABSTRACT
The Space Situational Awareness (SSA) problem is becoming an exponentially
significant concern for satellite operators. The threat of on-orbit collisions endangers
satellites, spacecrafts and astronauts themselves especially in low-earth orbits
(LEO). Many collisions occurred between satellites and debris that include natural,
operational and non-operational objects in space. The collision between Russian
cosmos 2251 and American iridium 33, for instance, imposed the need for an
accurate orbital propagation module. In order to perform successful collision
avoidance maneuvers, the mission operators need the orbit prediction to be highly
accurate. Simple impractical number of collision avoidance maneuvers represents
dreadful solution to escape of collision. Fake warning means waste of fuel and
resources of satellite. This paper introduces an enhanced model to increase the
accuracy of propagation estimation based on a precise perturbation model.

DOI

10.21608/amme.2018.34732

Keywords

Orbit, propagation, Drag, TLE, Cowell, STK, SGP4, hpop, eclipse, ephemerides

Authors

First Name

A.

Last Name

Refaat

MiddleName

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Affiliation

Egyptian Armed Forces.

Email

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Orcid

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First Name

A.

Last Name

Badawy

MiddleName

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Affiliation

Assoc. Prof., October University for Modern Sciences and Arts (MSA), Egypt.

Email

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City

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Orcid

-

First Name

M.

Last Name

Ashry

MiddleName

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Affiliation

Egyptian Armed Forces.

Email

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City

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Orcid

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First Name

Adel

Last Name

Omar

MiddleName

-

Affiliation

Egyptian Armed Forces.

Email

-

City

-

Orcid

-

Volume

18

Article Issue

18th International Conference on Applied Mechanics and Mechanical Engineering.

Related Issue

5736

Issue Date

2018-04-01

Receive Date

2019-06-13

Publish Date

2018-04-01

Page Start

1

Page End

9

Print ISSN

2636-4352

Online ISSN

2636-4360

Link

https://amme.journals.ekb.eg/article_34732.html

Detail API

https://amme.journals.ekb.eg/service?article_code=34732

Order

16

Type

Original Article

Type Code

831

Publication Type

Journal

Publication Title

The International Conference on Applied Mechanics and Mechanical Engineering

Publication Link

https://amme.journals.ekb.eg/

MainTitle

HIGH ACCURACY SPACECRAFT ORBIT PROPAGATOR VALIDATION

Details

Type

Article

Created At

22 Jan 2023