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Long term nonlinear propagation of uncertainties in perturbed geocentric dynamics using automatic domain splitting

Long term nonlinear propagation of uncertainties in perturbed geocentric dynamics using automatic domain splitting
Long term nonlinear propagation of uncertainties in perturbed geocentric dynamics using automatic domain splitting
Current approaches to uncertainty propagation in astrodynamics mainly refer to
linearized models or Monte Carlo simulations. Naive linear methods fail in nonlinear dynamics, whereas Monte Carlo simulations tend to be computationally
intensive. Differential algebra has already proven to be an efficient compromise
by replacing thousands of pointwise integrations of Monte Carlo runs with the
fast evaluation of the arbitrary order Taylor expansion of the flow of the dynamics. However, the current implementation of the DA-based high-order uncertainty propagator fails in highly nonlinear dynamics or long term propagation. We solve this issue by introducing automatic domain splitting. During propagation, the polynomial of the current state is split in two polynomials when its accuracy reaches a given threshold. The resulting polynomials accurately track uncertainties, even in highly nonlinear dynamics and long term propagations. Furthermore, valuable additional information about the dynamical system is available from the pattern in which those automatic splits occur. From this pattern it is immediately visible where the system behaves chaotically and where its evolution is smooth. Furthermore, it is possible to deduce the behavior of the system for each region, yielding further insight into the dynamics. In this work, the method is applied to the analysis of an end-of-life disposal trajectory of the INTEGRAL spacecraft.
1-20
Wittig, Alexander
3a140128-b118-4b8c-9856-a0d4f390b201
Di Lizia, Pierluigi
f86916ba-a73b-42a9-8247-558335c21f22
Armellin, Roberto
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Bernelli-Zazzera, Franco
4b3eb3b1-d06e-47cd-9676-f465dba2b1e7
Makino, Kyoko
273d1542-a2f6-4c1a-b54c-7a5a493151a0
Berz, Martin
f8159a81-aa52-4ba3-8b8f-a672aec96b47
Wittig, Alexander
3a140128-b118-4b8c-9856-a0d4f390b201
Di Lizia, Pierluigi
f86916ba-a73b-42a9-8247-558335c21f22
Armellin, Roberto
61950d5c-3dcf-45f5-b391-7e8c6ffb8e6f
Bernelli-Zazzera, Franco
4b3eb3b1-d06e-47cd-9676-f465dba2b1e7
Makino, Kyoko
273d1542-a2f6-4c1a-b54c-7a5a493151a0
Berz, Martin
f8159a81-aa52-4ba3-8b8f-a672aec96b47

Wittig, Alexander, Di Lizia, Pierluigi, Armellin, Roberto, Bernelli-Zazzera, Franco, Makino, Kyoko and Berz, Martin (2014) Long term nonlinear propagation of uncertainties in perturbed geocentric dynamics using automatic domain splitting. 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014, , Rome, Italy. 24 - 26 Mar 2014. pp. 1-20 .

Record type: Conference or Workshop Item (Paper)

Abstract

Current approaches to uncertainty propagation in astrodynamics mainly refer to
linearized models or Monte Carlo simulations. Naive linear methods fail in nonlinear dynamics, whereas Monte Carlo simulations tend to be computationally
intensive. Differential algebra has already proven to be an efficient compromise
by replacing thousands of pointwise integrations of Monte Carlo runs with the
fast evaluation of the arbitrary order Taylor expansion of the flow of the dynamics. However, the current implementation of the DA-based high-order uncertainty propagator fails in highly nonlinear dynamics or long term propagation. We solve this issue by introducing automatic domain splitting. During propagation, the polynomial of the current state is split in two polynomials when its accuracy reaches a given threshold. The resulting polynomials accurately track uncertainties, even in highly nonlinear dynamics and long term propagations. Furthermore, valuable additional information about the dynamical system is available from the pattern in which those automatic splits occur. From this pattern it is immediately visible where the system behaves chaotically and where its evolution is smooth. Furthermore, it is possible to deduce the behavior of the system for each region, yielding further insight into the dynamics. In this work, the method is applied to the analysis of an end-of-life disposal trajectory of the INTEGRAL spacecraft.

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IAA-AAS-DyCoSS2-05-04.pdf - Accepted Manuscript
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More information

Published date: 24 March 2014
Venue - Dates: 2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014, , Rome, Italy, 2014-03-24 - 2014-03-26
Organisations: Astronautics Group

Identifiers

Local EPrints ID: 366764
URI: http://eprints.soton.ac.uk/id/eprint/366764
PURE UUID: d0e5ece2-6249-4b76-adfd-9e50f0535bf8
ORCID for Alexander Wittig: ORCID iD orcid.org/0000-0002-4594-0368

Catalogue record

Date deposited: 10 Jul 2014 10:18
Last modified: 15 Mar 2024 03:58

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Contributors

Author: Pierluigi Di Lizia
Author: Franco Bernelli-Zazzera
Author: Kyoko Makino
Author: Martin Berz

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