Solar radiation pressure Hamiltonian feedback control for unstable Libation Point Orbis
Solar radiation pressure Hamiltonian feedback control for unstable Libation Point Orbis
This work investigates a Hamiltonian structure-preserving control that uses the acceleration of solar radiation pressure for the stabilization of unstable periodic orbits in the circular restricted three-body problem. This control aims to stabilize the libration-point orbits in the sense of Lyapunov by achieving simple stability. It also preserves the Hamiltonian nature of the controlled system. The Hamiltonian structure-preserving control is then extended to a general case in which complex and conjugate eigenvalues occur at high-amplitude orbits. High-amplitude orbits are currently of interest to the European Space Agency for future libration-point orbit missions because they require a lower insertion Δv compared to low-amplitude orbits. Based on the design of the feedback control, the purpose of this work is to verify when the use of solar radiation pressure is feasible and to determine the structural requirements and the spacecraft’s pointing accuracy.
Soldini, S.
bfa90841-1048-4104-a330-b855f1e6eea5
Colombo, C.
9bf7fbdc-abab-4f6e-823a-a8b4ec9663b3
Walker, Scott
f28a342f-9755-48fd-94ea-09e44ac4dbf5
17 March 2017
Soldini, S.
bfa90841-1048-4104-a330-b855f1e6eea5
Colombo, C.
9bf7fbdc-abab-4f6e-823a-a8b4ec9663b3
Walker, Scott
f28a342f-9755-48fd-94ea-09e44ac4dbf5
Soldini, S., Colombo, C. and Walker, Scott
(2017)
Solar radiation pressure Hamiltonian feedback control for unstable Libation Point Orbis.
Journal of Guidance, Control, and Dynamics, 40 (6).
(doi:10.2514/1.G002090).
Abstract
This work investigates a Hamiltonian structure-preserving control that uses the acceleration of solar radiation pressure for the stabilization of unstable periodic orbits in the circular restricted three-body problem. This control aims to stabilize the libration-point orbits in the sense of Lyapunov by achieving simple stability. It also preserves the Hamiltonian nature of the controlled system. The Hamiltonian structure-preserving control is then extended to a general case in which complex and conjugate eigenvalues occur at high-amplitude orbits. High-amplitude orbits are currently of interest to the European Space Agency for future libration-point orbit missions because they require a lower insertion Δv compared to low-amplitude orbits. Based on the design of the feedback control, the purpose of this work is to verify when the use of solar radiation pressure is feasible and to determine the structural requirements and the spacecraft’s pointing accuracy.
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Published date: 17 March 2017
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Copyright © 2016 by S. Soldini et al. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com
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Local EPrints ID: 471216
URI: http://eprints.soton.ac.uk/id/eprint/471216
ISSN: 0731-5090
PURE UUID: 7b41d574-a5e9-4620-9867-1652bfb369d9
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Date deposited: 31 Oct 2022 18:08
Last modified: 16 Mar 2024 22:08
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Author:
S. Soldini
Author:
C. Colombo
Author:
Scott Walker
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