Extended kalman filtering in regularized coordinates for orbit determination

David Ciliberto, Puneet Singla, Manoranjan Majji

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The linear error theory used in our previous work developing an extended Kalman filter formulation in Burdet regularized coordinates for the purpose of estimating the unperturbed two-body motion of Earth-orbiting satellites is improved upon. Critical challenges in implementation arise as a result of this formulation and are addressed. Simulated orbit determination is conducted in the regularized space and using a traditional Cartesian extended Kalman filter for comparison.

Original languageEnglish (US)
Title of host publicationSpaceflight Mechanics 2019
EditorsFrancesco Topputo, Andrew J. Sinclair, Matthew P. Wilkins, Renato Zanetti
PublisherUnivelt Inc.
Pages89-108
Number of pages20
ISBN (Print)9780877036593
Publication statusPublished - Jan 1 2019
Event29th AAS/AIAA Space Flight Mechanics Meeting, 2019 - Maui, United States
Duration: Jan 13 2019Jan 17 2019

Publication series

NameAdvances in the Astronautical Sciences
Volume168
ISSN (Print)0065-3438

Conference

Conference29th AAS/AIAA Space Flight Mechanics Meeting, 2019
CountryUnited States
CityMaui
Period1/13/191/17/19

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All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Ciliberto, D., Singla, P., & Majji, M. (2019). Extended kalman filtering in regularized coordinates for orbit determination. In F. Topputo, A. J. Sinclair, M. P. Wilkins, & R. Zanetti (Eds.), Spaceflight Mechanics 2019 (pp. 89-108). [AAS 19-513] (Advances in the Astronautical Sciences; Vol. 168). Univelt Inc..