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Bibliographic Details
Main Authors: Semeraro, Simone, Kolmanovsky, Ilya, Garone, Emanuele
Format: Preprint
Published: 2024
Subjects:
Online Access:https://arxiv.org/abs/2407.16389
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author Semeraro, Simone
Kolmanovsky, Ilya
Garone, Emanuele
author_facet Semeraro, Simone
Kolmanovsky, Ilya
Garone, Emanuele
contents The paper revisits a Lyapunov-based feedback control to implement spacecraft orbital transfer maneuvers. The spacecraft equations of motion in the form of Gauss Variational Equations (GVEs) are used. By shaping the Lyapunov function using barrier functions, we demonstrate that state and control constraints during orbital maneuvers can be enforced. Simulation results from orbital maneuvering scenarios are reported. The synergistic use of the reference governor in conjunction with the barrier functions is proposed to ensure convergence to the target orbit (liveness) while satisfying the imposed constraints.
format Preprint
id arxiv_https___arxiv_org_abs_2407_16389
institution arXiv
publishDate 2024
record_format arxiv
spellingShingle On Constrained Feedback Control of Spacecraft Orbital Transfer Maneuvers
Semeraro, Simone
Kolmanovsky, Ilya
Garone, Emanuele
Optimization and Control
The paper revisits a Lyapunov-based feedback control to implement spacecraft orbital transfer maneuvers. The spacecraft equations of motion in the form of Gauss Variational Equations (GVEs) are used. By shaping the Lyapunov function using barrier functions, we demonstrate that state and control constraints during orbital maneuvers can be enforced. Simulation results from orbital maneuvering scenarios are reported. The synergistic use of the reference governor in conjunction with the barrier functions is proposed to ensure convergence to the target orbit (liveness) while satisfying the imposed constraints.
title On Constrained Feedback Control of Spacecraft Orbital Transfer Maneuvers
topic Optimization and Control
url https://arxiv.org/abs/2407.16389