Computing the critical points of the distance function between two Keplerian orbits via rigorous global optimization
Computing the critical points of the distance function between two Keplerian orbits via rigorous global optimization
A novel method to compute all critical points of the distance function between two Keplerian orbits (either bounded or unbounded) with a common focus is presented. The problem is attacked as a global optimization problem, solved by a rigorous global optimizer based on Taylor models. Thus, thigh enclosures of the stationary points are obtained. The embedded capability of the method of delivering high-order Taylor expansions is then used to analyze how uncertain orbital parameters affect the position of the stationary points and the associated distance values. Sample orbital sets and Apophis asteroid are used as test cases
377-395
Armellin, R.
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Lizia, P. Di
ee47f1b1-2131-4e5d-a18d-c67142d43bc5
Berz, M.
95c4e8a8-e1d9-4ad7-91c6-2832b7a1dd02
Makino, K.
833360d9-db7d-42ac-b184-98c31b0c9fe0
July 2010
Armellin, R.
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Lizia, P. Di
ee47f1b1-2131-4e5d-a18d-c67142d43bc5
Berz, M.
95c4e8a8-e1d9-4ad7-91c6-2832b7a1dd02
Makino, K.
833360d9-db7d-42ac-b184-98c31b0c9fe0
Armellin, R., Lizia, P. Di, Berz, M. and Makino, K.
(2010)
Computing the critical points of the distance function between two Keplerian orbits via rigorous global optimization.
Celestial Mechanics and Dynamical Astronomy, 107 (3), .
(doi:10.1007/s10569-010-9281-7).
Abstract
A novel method to compute all critical points of the distance function between two Keplerian orbits (either bounded or unbounded) with a common focus is presented. The problem is attacked as a global optimization problem, solved by a rigorous global optimizer based on Taylor models. Thus, thigh enclosures of the stationary points are obtained. The embedded capability of the method of delivering high-order Taylor expansions is then used to analyze how uncertain orbital parameters affect the position of the stationary points and the associated distance values. Sample orbital sets and Apophis asteroid are used as test cases
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Published date: July 2010
Organisations:
Aeronautics, Astronautics & Comp. Eng
Identifiers
Local EPrints ID: 360603
URI: http://eprints.soton.ac.uk/id/eprint/360603
ISSN: 0923-2958
PURE UUID: 5e0a049b-f950-4ac9-9124-fb859e7d7cc7
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Date deposited: 16 Dec 2013 13:09
Last modified: 14 Mar 2024 15:40
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Author:
P. Di Lizia
Author:
M. Berz
Author:
K. Makino
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