Inertial space-based orbit estimation: A new measurement model for multiple observers-Reference-Cited by-同舟云学术

Inertial space-based orbit estimation: A new measurement model for multiple observers

Published:2021-04 Issue: Volume:181 Page:717-732
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Hippelheuser James^ORCID,Elgohary Tarek A.^ORCID

Funder

Florida Space Grant Consortium

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. Theory of Orbit Determination. Part I: Classical Methods;Anderson,1963

2. Laplacian orbit determination and differential corrections;Branham;Celestial Mech. Dyn. Astron.,2005

3. Methods of Orbit Determination;Escobal,1965

4. A new procedure for the solution of the classical problem of minimal orbit determination from three lines of sight;Gooding;Celestial Mech. Dyn. Astron.,1996

5. A performance based comparison of angle-only initial orbit determination methods;Karimi;Advances in Astronautical Sciences, AAS/AIAA, Hilton Head Island, South Carolina,2013

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