Forecasting satellite trajectories by interpolating hybrid orbit propagators
Forecasting satellite trajectories by interpolating hybrid orbit propagators
A hybrid orbit propagator based on the analytical integration of the Kepler problem is designed to determine the future position and velocity of any orbiter, usually an artificial satellite or space debris fragment, in two steps: an initial approximation generated by means of an integration method, followed by a forecast of its error, determined by a prediction technique that models and reproduces the missing dynamics. In this study we analyze the effect of slightly changing the initial conditions for which a hybrid propagator was developed. We explore the possibility of generating a new hybrid propagator from others previously developed for nearby initial conditions. We find that the interpolation of the parameters of the prediction technique, which in this case is an additive Holt-Winters method, yields similarly accurate results to a non-interpolated hybrid propagator when modeling the J2 effect in the main problem propagation.
650-661
Pérez, Iván
7a625bcb-123e-42cc-b7cf-c9c1128b5ecd
San-Martín, Montserrat
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López, Rosario
c1a34557-f092-40ba-b697-82da7ca298c5
Vergara, Eliseo P.
eff9c7c3-dadd-4d20-8c1a-077f80ae0092
Wittig, Alexander
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San-Juan, Juan Félix
eea5508b-dc4e-4cda-aaa3-765b69955df7
2017
Pérez, Iván
7a625bcb-123e-42cc-b7cf-c9c1128b5ecd
San-Martín, Montserrat
d99bc99b-d0c4-4acd-a56d-dacb362ab33b
López, Rosario
c1a34557-f092-40ba-b697-82da7ca298c5
Vergara, Eliseo P.
eff9c7c3-dadd-4d20-8c1a-077f80ae0092
Wittig, Alexander
3a140128-b118-4b8c-9856-a0d4f390b201
San-Juan, Juan Félix
eea5508b-dc4e-4cda-aaa3-765b69955df7
Pérez, Iván, San-Martín, Montserrat, López, Rosario, Vergara, Eliseo P., Wittig, Alexander and San-Juan, Juan Félix
(2017)
Forecasting satellite trajectories by interpolating hybrid orbit propagators.
Martinez de Pison, F., Urraca, R., Quintian, H. and Corchado, E.
(eds.)
In Hybrid Artificial Intelligent Systems - 12th International Conference, HAIS 2017, Proceedings.
vol. 10334,
Springer.
.
(doi:10.1007/978-3-319-59650-1_55).
Record type:
Conference or Workshop Item
(Paper)
Abstract
A hybrid orbit propagator based on the analytical integration of the Kepler problem is designed to determine the future position and velocity of any orbiter, usually an artificial satellite or space debris fragment, in two steps: an initial approximation generated by means of an integration method, followed by a forecast of its error, determined by a prediction technique that models and reproduces the missing dynamics. In this study we analyze the effect of slightly changing the initial conditions for which a hybrid propagator was developed. We explore the possibility of generating a new hybrid propagator from others previously developed for nearby initial conditions. We find that the interpolation of the parameters of the prediction technique, which in this case is an additive Holt-Winters method, yields similarly accurate results to a non-interpolated hybrid propagator when modeling the J2 effect in the main problem propagation.
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e-pub ahead of print date: 2 June 2017
Published date: 2017
Venue - Dates:
12th International Conference on Hybrid Artificial Intelligent Systems, HAIS 2017, , La Rioja, Spain, 2017-06-21 - 2017-06-23
Identifiers
Local EPrints ID: 419788
URI: http://eprints.soton.ac.uk/id/eprint/419788
ISSN: 0302-9743
PURE UUID: 28744c6c-32d4-4a39-b35f-07544930339e
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Date deposited: 20 Apr 2018 16:30
Last modified: 06 Jun 2024 01:59
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Contributors
Author:
Iván Pérez
Author:
Montserrat San-Martín
Author:
Rosario López
Author:
Eliseo P. Vergara
Author:
Juan Félix San-Juan
Editor:
F. Martinez de Pison
Editor:
R. Urraca
Editor:
H. Quintian
Editor:
E. Corchado
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