Equal distribution of satellite constellations on circular target orbits

Ewoud Vos; Jacquelien M.A. Scherpen; A. J. van der Schaft

doi:10.1016/j.automatica.2014.08.027

Equal distribution of satellite constellations on circular target orbits

Ewoud Vos, Jacquelien M.A. Scherpen, A. J. van der Schaft

University of Groningen, Faculty of Mathematics and Natural Sciences

Research output: Contribution to journal › Article › Academic › peer-review

Abstract

This paper addresses the problem of equal distribution of satellite constellations on circular target orbits. The control goal is to make the constellation converge to a circular target orbit, while spatially distributing the satellites at equal inter-satellite distances. The solution is defined in the port-Hamiltonian framework, which gives a clear physical interpretation of the obtained control laws, insight into the energy consumption and complete stability proofs. The controller consists of two parts: the internal control system steers each individual satellite to the target orbit, the external control system equally distributes the satellite constellation. Numerical simulation results are given to illustrate the effectiveness of the approach. (C) 2014 Elsevier Ltd. All rights reserved.

Original language	English
Pages (from-to)	2641-2647
Number of pages	7
Journal	Automatica
Volume	50
Issue number	10
DOIs	https://doi.org/10.1016/j.automatica.2014.08.027
Publication status	Published - 1 Oct 2014
Externally published	Yes

Keywords

multi-agent systems
asymptotic stabilization
guidance
navigation and control of vehicles
mission control and operations
Port-Hamiltonian systems
distributed control
hamiltonian-systems

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10.1016/j.automatica.2014.08.027

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title = "Equal distribution of satellite constellations on circular target orbits",

abstract = "This paper addresses the problem of equal distribution of satellite constellations on circular target orbits. The control goal is to make the constellation converge to a circular target orbit, while spatially distributing the satellites at equal inter-satellite distances. The solution is defined in the port-Hamiltonian framework, which gives a clear physical interpretation of the obtained control laws, insight into the energy consumption and complete stability proofs. The controller consists of two parts: the internal control system steers each individual satellite to the target orbit, the external control system equally distributes the satellite constellation. Numerical simulation results are given to illustrate the effectiveness of the approach. (C) 2014 Elsevier Ltd. All rights reserved.",

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T1 - Equal distribution of satellite constellations on circular target orbits

AU - Vos, Ewoud

AU - Scherpen, Jacquelien M.A.

AU - van der Schaft, A. J.

PY - 2014/10/1

Y1 - 2014/10/1

N2 - This paper addresses the problem of equal distribution of satellite constellations on circular target orbits. The control goal is to make the constellation converge to a circular target orbit, while spatially distributing the satellites at equal inter-satellite distances. The solution is defined in the port-Hamiltonian framework, which gives a clear physical interpretation of the obtained control laws, insight into the energy consumption and complete stability proofs. The controller consists of two parts: the internal control system steers each individual satellite to the target orbit, the external control system equally distributes the satellite constellation. Numerical simulation results are given to illustrate the effectiveness of the approach. (C) 2014 Elsevier Ltd. All rights reserved.

AB - This paper addresses the problem of equal distribution of satellite constellations on circular target orbits. The control goal is to make the constellation converge to a circular target orbit, while spatially distributing the satellites at equal inter-satellite distances. The solution is defined in the port-Hamiltonian framework, which gives a clear physical interpretation of the obtained control laws, insight into the energy consumption and complete stability proofs. The controller consists of two parts: the internal control system steers each individual satellite to the target orbit, the external control system equally distributes the satellite constellation. Numerical simulation results are given to illustrate the effectiveness of the approach. (C) 2014 Elsevier Ltd. All rights reserved.

KW - multi-agent systems

KW - asymptotic stabilization

KW - guidance

KW - navigation and control of vehicles

KW - mission control and operations

KW - Port-Hamiltonian systems

KW - distributed control

KW - hamiltonian-systems

KW - multi-agent systemen

KW - asymptotische stabilisatie

KW - begeleiding

KW - navigatie en besturing van voertuigen

KW - missiecontrole en operaties

KW - port-Hamiltoniaanse systemen

KW - gedistribueerde controle

KW - Hamiltoniaanse systemen

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DO - 10.1016/j.automatica.2014.08.027

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VL - 50

SP - 2641

EP - 2647

JO - Automatica

JF - Automatica

IS - 10

ER -

Equal distribution of satellite constellations on circular target orbits

Abstract

Keywords

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