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Stability analysis of three-dimensional quasi-satellite orbits around Phobos

Stability analysis of three-dimensional quasi-satellite orbits around Phobos
Stability analysis of three-dimensional quasi-satellite orbits around Phobos

The exploration to Martian moons is of growing interest with several space missions proposed to return samples from these bodies. The proximity operation planning needs to consider the complex dynamical environment. The purpose of the present work is to identify three-dimensional quasi-satellite orbits (3D QSO) around Phobos that are suitable for global mapping and bounded in the realistic model for a permissible period (i.e. 7 days). Linear stability and deviation indices are defined to indicate the safety of the orbit for operations. Periodic resonant 3D QSO are first computed in the circular-restricted three-body problem (CR3BP) based on the approach of bifurcation and continuation. Bifurcations are identified along the continuation curve. A skipping routine is used to recover solutions with high z-amplitudes. The 3D QSO obtained in the CR3BP serves as a database of initial guesses for bounded orbits in the realistic model and leads to a picture of the stability region. Stable solutions with high z-amplitudes (e.g. up to 40 km at x-amplitude = 30 km) are found in this stage. As the CR3BP is a simplified model, the eccentricity and higher-order gravity terms can strongly perturb the orbits in the realistic model. Orbit stability is assessed by a validation model that considers Phobos moves in the Mars J2-perturbed elliptic orbit. With the validation model a picture of orbit robustness to the initial phase can be quickly generated. Orbits that are always bounded regardless of the initial phase are identified. Those promising orbits are then verified in the realistic model starting from varied epochs. For instance, an always bounded orbit of favorable characteristics has an x-amplitude of 24 km and an inclination of 38°.

Martian moons exploration, Quasi-satellite orbits, Resonant periodic orbits, Stability analysis
7716-7725
International Astronautical Federation
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Canalias, Elisabet
900c6845-45ee-4422-b21b-810d5f27f21d
Hestroffer, Daniel
06b8b68f-3a94-4f2e-b434-ce6822b08c71
Hou, Xiyun
f0b359ce-3eeb-4950-9523-88bc4f16b931
Chen, Hongru
8286469d-afe1-46e5-b107-694017de4d97
Canalias, Elisabet
900c6845-45ee-4422-b21b-810d5f27f21d
Hestroffer, Daniel
06b8b68f-3a94-4f2e-b434-ce6822b08c71
Hou, Xiyun
f0b359ce-3eeb-4950-9523-88bc4f16b931

Chen, Hongru, Canalias, Elisabet, Hestroffer, Daniel and Hou, Xiyun (2018) Stability analysis of three-dimensional quasi-satellite orbits around Phobos. In 69th International Astronautical Congress (IAC 2018): Involving Everyone. International Astronautical Federation. pp. 7716-7725 .

Record type: Conference or Workshop Item (Paper)

Abstract

The exploration to Martian moons is of growing interest with several space missions proposed to return samples from these bodies. The proximity operation planning needs to consider the complex dynamical environment. The purpose of the present work is to identify three-dimensional quasi-satellite orbits (3D QSO) around Phobos that are suitable for global mapping and bounded in the realistic model for a permissible period (i.e. 7 days). Linear stability and deviation indices are defined to indicate the safety of the orbit for operations. Periodic resonant 3D QSO are first computed in the circular-restricted three-body problem (CR3BP) based on the approach of bifurcation and continuation. Bifurcations are identified along the continuation curve. A skipping routine is used to recover solutions with high z-amplitudes. The 3D QSO obtained in the CR3BP serves as a database of initial guesses for bounded orbits in the realistic model and leads to a picture of the stability region. Stable solutions with high z-amplitudes (e.g. up to 40 km at x-amplitude = 30 km) are found in this stage. As the CR3BP is a simplified model, the eccentricity and higher-order gravity terms can strongly perturb the orbits in the realistic model. Orbit stability is assessed by a validation model that considers Phobos moves in the Mars J2-perturbed elliptic orbit. With the validation model a picture of orbit robustness to the initial phase can be quickly generated. Orbits that are always bounded regardless of the initial phase are identified. Those promising orbits are then verified in the realistic model starting from varied epochs. For instance, an always bounded orbit of favorable characteristics has an x-amplitude of 24 km and an inclination of 38°.

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More information

Published date: 2018
Venue - Dates: 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018, , Bremen, Germany, 2018-10-01 - 2018-10-05
Keywords: Martian moons exploration, Quasi-satellite orbits, Resonant periodic orbits, Stability analysis

Identifiers

Local EPrints ID: 490998
URI: http://eprints.soton.ac.uk/id/eprint/490998
PURE UUID: 6f2e332b-dd09-42fb-a69d-2b4103999cb4
ORCID for Hongru Chen: ORCID iD orcid.org/0000-0001-9453-6962

Catalogue record

Date deposited: 11 Jun 2024 16:34
Last modified: 12 Jun 2024 02:11

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Contributors

Author: Hongru Chen ORCID iD
Author: Elisabet Canalias
Author: Daniel Hestroffer
Author: Xiyun Hou

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