Station Keeping of Constellations Using Multiobjective Strategies

The goal of the present paper is to study the problem of station keeping maneuvers of satellites that belong to a constellation. The objective is to perform those maneuvers with low fuel consumption and but also including a time constraint. This type of problem has several aspects to be considered,...

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Main Authors: Evandro Marconi Rocco, Marcelo Lopes de Oliveira e Souza, Antonio Fernando Bertachini de Almeida Prado
Format: Article
Language:English
Published: Hindawi Limited 2013-01-01
Series:Mathematical Problems in Engineering
Online Access:http://dx.doi.org/10.1155/2013/476451
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spelling doaj-8b567d1509864e6992802868199ae66b2020-11-24T20:54:59ZengHindawi LimitedMathematical Problems in Engineering1024-123X1563-51472013-01-01201310.1155/2013/476451476451Station Keeping of Constellations Using Multiobjective StrategiesEvandro Marconi Rocco0Marcelo Lopes de Oliveira e Souza1Antonio Fernando Bertachini de Almeida Prado2DMC, Space Mechanics and Control Division, National Institute for Space Research (INPE), Avenida dos Astronautas 1758, 12227-010 São José dos Campos, SP, BrazilDMC, Space Mechanics and Control Division, National Institute for Space Research (INPE), Avenida dos Astronautas 1758, 12227-010 São José dos Campos, SP, BrazilDMC, Space Mechanics and Control Division, National Institute for Space Research (INPE), Avenida dos Astronautas 1758, 12227-010 São José dos Campos, SP, BrazilThe goal of the present paper is to study the problem of station keeping maneuvers of satellites that belong to a constellation. The objective is to perform those maneuvers with low fuel consumption and but also including a time constraint. This type of problem has several aspects to be considered, like fuel consumption, duration of the maneuvers. These aspects are applied to all the satellites of the constellation, so a strategy has to be found to consider the global optimization of those variables that can control the geometry of the constellation. So, this is a multiobjective problem. To find a solution, strategies are formulated that minimize the fuel consumption considering all the satellites and also considering the duration of the maneuver. Numerical examples are shown.http://dx.doi.org/10.1155/2013/476451
collection DOAJ
language English
format Article
sources DOAJ
author Evandro Marconi Rocco
Marcelo Lopes de Oliveira e Souza
Antonio Fernando Bertachini de Almeida Prado
spellingShingle Evandro Marconi Rocco
Marcelo Lopes de Oliveira e Souza
Antonio Fernando Bertachini de Almeida Prado
Station Keeping of Constellations Using Multiobjective Strategies
Mathematical Problems in Engineering
author_facet Evandro Marconi Rocco
Marcelo Lopes de Oliveira e Souza
Antonio Fernando Bertachini de Almeida Prado
author_sort Evandro Marconi Rocco
title Station Keeping of Constellations Using Multiobjective Strategies
title_short Station Keeping of Constellations Using Multiobjective Strategies
title_full Station Keeping of Constellations Using Multiobjective Strategies
title_fullStr Station Keeping of Constellations Using Multiobjective Strategies
title_full_unstemmed Station Keeping of Constellations Using Multiobjective Strategies
title_sort station keeping of constellations using multiobjective strategies
publisher Hindawi Limited
series Mathematical Problems in Engineering
issn 1024-123X
1563-5147
publishDate 2013-01-01
description The goal of the present paper is to study the problem of station keeping maneuvers of satellites that belong to a constellation. The objective is to perform those maneuvers with low fuel consumption and but also including a time constraint. This type of problem has several aspects to be considered, like fuel consumption, duration of the maneuvers. These aspects are applied to all the satellites of the constellation, so a strategy has to be found to consider the global optimization of those variables that can control the geometry of the constellation. So, this is a multiobjective problem. To find a solution, strategies are formulated that minimize the fuel consumption considering all the satellites and also considering the duration of the maneuver. Numerical examples are shown.
url http://dx.doi.org/10.1155/2013/476451
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