Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite

Murat Bagci; Cengiz Hacizade

doi:10.1109/RAST.2015.7208437

Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite

Murat Bagci, Cengiz Hacizade

Department of Aeronautical Engineering

Turkish Air Force Academy

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

5 Citations (Scopus)

Abstract

Determination and control of the satellite's orbit is acting vital role on space mission. Accuracy in calculations for position and velocity of such a satellite is important for fulfilling the tasks. The motion of a Low Earth Orbit (LEO) satellite can be modelled with Keplerian equations. In this study, we use Keplerian equations to construct dynamic model of LEO satellite and analyze performances of three numerical methods (Newton-Raphson, Bancroft and Matlab fsolve) in Global Positioning System (GPS) based trilateration problem solving.

Original language	English
Title of host publication	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies
Editors	M. Fevzi Unal, Suleyman Basturk, Okyay Kaynak, Abdurrahman Hacioglu, Fuat Ince
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	731-735
Number of pages	5
ISBN (Electronic)	9781467377607
DOIs	https://doi.org/10.1109/RAST.2015.7208437
Publication status	Published - 17 Aug 2015
Event	7th International Conference on Recent Advances in Space Technologies, RAST 2015 - Istanbul, Turkey Duration: 16 Jun 2015 → 19 Jun 2015

Publication series

Name	RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

Conference

Conference	7th International Conference on Recent Advances in Space Technologies, RAST 2015
Country/Territory	Turkey
City	Istanbul
Period	16/06/15 → 19/06/15

Bibliographical note

Publisher Copyright:
© 2015 IEEE.

Keywords

Bancroft
GPS
Matlab fsolve
Newton-Raphson

Access to Document

10.1109/RAST.2015.7208437

Cite this

Bagci, M., & Hacizade, C. (2015). Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite. In M. F. Unal, S. Basturk, O. Kaynak, A. Hacioglu, & F. Ince (Eds.), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies (pp. 731-735). Article 7208437 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/RAST.2015.7208437

Bagci, Murat ; Hacizade, Cengiz. / Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite. RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. editor / M. Fevzi Unal ; Suleyman Basturk ; Okyay Kaynak ; Abdurrahman Hacioglu ; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. pp. 731-735 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

@inproceedings{234f11ca7ecb4f519c7a9adbce4425f4,

title = "Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite",

abstract = "Determination and control of the satellite's orbit is acting vital role on space mission. Accuracy in calculations for position and velocity of such a satellite is important for fulfilling the tasks. The motion of a Low Earth Orbit (LEO) satellite can be modelled with Keplerian equations. In this study, we use Keplerian equations to construct dynamic model of LEO satellite and analyze performances of three numerical methods (Newton-Raphson, Bancroft and Matlab fsolve) in Global Positioning System (GPS) based trilateration problem solving.",

keywords = "Bancroft, GPS, Matlab fsolve, Newton-Raphson",

author = "Murat Bagci and Cengiz Hacizade",

note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 7th International Conference on Recent Advances in Space Technologies, RAST 2015 ; Conference date: 16-06-2015 Through 19-06-2015",

year = "2015",

month = aug,

day = "17",

doi = "10.1109/RAST.2015.7208437",

language = "English",

series = "RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies",

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

pages = "731--735",

editor = "Unal, {M. Fevzi} and Suleyman Basturk and Okyay Kaynak and Abdurrahman Hacioglu and Fuat Ince",

booktitle = "RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies",

address = "United States",

}

Bagci, M & Hacizade, C 2015, Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite. in MF Unal, S Basturk, O Kaynak, A Hacioglu & F Ince (eds), RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies., 7208437, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies, Institute of Electrical and Electronics Engineers Inc., pp. 731-735, 7th International Conference on Recent Advances in Space Technologies, RAST 2015, Istanbul, Turkey, 16/06/15. https://doi.org/10.1109/RAST.2015.7208437

Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite. / Bagci, Murat; Hacizade, Cengiz.
RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. ed. / M. Fevzi Unal; Suleyman Basturk; Okyay Kaynak; Abdurrahman Hacioglu; Fuat Ince. Institute of Electrical and Electronics Engineers Inc., 2015. p. 731-735 7208437 (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite

AU - Bagci, Murat

AU - Hacizade, Cengiz

PY - 2015/8/17

Y1 - 2015/8/17

N2 - Determination and control of the satellite's orbit is acting vital role on space mission. Accuracy in calculations for position and velocity of such a satellite is important for fulfilling the tasks. The motion of a Low Earth Orbit (LEO) satellite can be modelled with Keplerian equations. In this study, we use Keplerian equations to construct dynamic model of LEO satellite and analyze performances of three numerical methods (Newton-Raphson, Bancroft and Matlab fsolve) in Global Positioning System (GPS) based trilateration problem solving.

AB - Determination and control of the satellite's orbit is acting vital role on space mission. Accuracy in calculations for position and velocity of such a satellite is important for fulfilling the tasks. The motion of a Low Earth Orbit (LEO) satellite can be modelled with Keplerian equations. In this study, we use Keplerian equations to construct dynamic model of LEO satellite and analyze performances of three numerical methods (Newton-Raphson, Bancroft and Matlab fsolve) in Global Positioning System (GPS) based trilateration problem solving.

KW - Bancroft

KW - GPS

KW - Matlab fsolve

KW - Newton-Raphson

UR - http://www.scopus.com/inward/record.url?scp=84959922090&partnerID=8YFLogxK

U2 - 10.1109/RAST.2015.7208437

DO - 10.1109/RAST.2015.7208437

M3 - Conference contribution

AN - SCOPUS:84959922090

T3 - RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

SP - 731

EP - 735

BT - RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies

A2 - Unal, M. Fevzi

A2 - Basturk, Suleyman

A2 - Kaynak, Okyay

A2 - Hacioglu, Abdurrahman

A2 - Ince, Fuat

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 7th International Conference on Recent Advances in Space Technologies, RAST 2015

Y2 - 16 June 2015 through 19 June 2015

ER -

Bagci M, Hacizade C. Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite. In Unal MF, Basturk S, Kaynak O, Hacioglu A, Ince F, editors, RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies. Institute of Electrical and Electronics Engineers Inc. 2015. p. 731-735. 7208437. (RAST 2015 - Proceedings of 7th International Conference on Recent Advances in Space Technologies). doi: 10.1109/RAST.2015.7208437

Performance analysis of GPS based orbit determination via numerical methods for a LEO satellite

Abstract

Publication series

Conference

Bibliographical note

Keywords

Access to Document

Other files and links

Fingerprint

Cite this