The University of Southampton
University of Southampton Institutional Repository

Dealing with uncertainties in angles-only initial orbit determination

Dealing with uncertainties in angles-only initial orbit determination
Dealing with uncertainties in angles-only initial orbit determination
A method to deal with uncertainties in initial orbit determination (IOD) is presented. This is based on the use of Taylor differential algebra (DA) to nonlinearly map uncertainties from the observation space to the state space. When a minimum set of observations is available, DA is used to expand the solution of the IOD problem in Taylor series with respect to measurement errors. When more observations are available, high order inversion tools are exploited to obtain full state pseudo-observations at a common epoch. The mean and covariance of these pseudo-observations are nonlinearly computed by evaluating the expectation of high order Taylor polynomials. Finally, a linear scheme is employed to update the current knowledge of the orbit. Angles-only observations are considered and simplified Keplerian dynamics adopted to ease the explanation. Three test cases of orbit determination of artificial satellites in different orbital regimes are presented to discuss the feature and performances of the proposed methodology.
0923-2958
1-16
Armellin, Roberto
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Di Lizia, Pierluigi
f86916ba-a73b-42a9-8247-558335c21f22
Zanetti, Renato
245aa251-d6d5-431a-8f8a-a21b992ccbe6
Armellin, Roberto
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Di Lizia, Pierluigi
f86916ba-a73b-42a9-8247-558335c21f22
Zanetti, Renato
245aa251-d6d5-431a-8f8a-a21b992ccbe6

Armellin, Roberto, Di Lizia, Pierluigi and Zanetti, Renato (2016) Dealing with uncertainties in angles-only initial orbit determination. Celestial Mechanics and Dynamical Astronomy, 1-16. (doi:10.1007/s10569-016-9694-z).

Record type: Article

Abstract

A method to deal with uncertainties in initial orbit determination (IOD) is presented. This is based on the use of Taylor differential algebra (DA) to nonlinearly map uncertainties from the observation space to the state space. When a minimum set of observations is available, DA is used to expand the solution of the IOD problem in Taylor series with respect to measurement errors. When more observations are available, high order inversion tools are exploited to obtain full state pseudo-observations at a common epoch. The mean and covariance of these pseudo-observations are nonlinearly computed by evaluating the expectation of high order Taylor polynomials. Finally, a linear scheme is employed to update the current knowledge of the orbit. Angles-only observations are considered and simplified Keplerian dynamics adopted to ease the explanation. Three test cases of orbit determination of artificial satellites in different orbital regimes are presented to discuss the feature and performances of the proposed methodology.

Text
PaperCelMecV2.pdf - Accepted Manuscript
Download (582kB)

More information

Accepted/In Press date: 5 April 2016
e-pub ahead of print date: 3 May 2016
Organisations: Astronautics Group

Identifiers

Local EPrints ID: 392035
URI: http://eprints.soton.ac.uk/id/eprint/392035
ISSN: 0923-2958
PURE UUID: 96fd727c-4c2f-4d20-8291-8cfd77c3e7d1

Catalogue record

Date deposited: 14 Apr 2016 08:59
Last modified: 15 Mar 2024 05:29

Export record

Altmetrics

Contributors

Author: Pierluigi Di Lizia
Author: Renato Zanetti

Download statistics

Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.

View more statistics

Atom RSS 1.0 RSS 2.0

Contact ePrints Soton: eprints@soton.ac.uk

ePrints Soton supports OAI 2.0 with a base URL of http://eprints.soton.ac.uk/cgi/oai2

This repository has been built using EPrints software, developed at the University of Southampton, but available to everyone to use.

We use cookies to ensure that we give you the best experience on our website. If you continue without changing your settings, we will assume that you are happy to receive cookies on the University of Southampton website.

×