Optimal design of the satellite constellation arrangement reconfiguration process

•A novel approach for reconfiguration of the satellite constellations is introduced.•Coupled non-simultaneous flight idea is presented to minimize reconfiguration phase.•Globally optimal solution is achieved by the efficient hybrid IWO/PSO technique. In this article, a novel approach is introduced f...

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Bibliographic Details
Published inAdvances in space research Vol. 58; no. 3; pp. 372 - 386
Main Authors Fakoor, Mahdi, Bakhtiari, Majid, Soleymani, Mahshid
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.08.2016
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ISSN0273-1177
1879-1948
DOI10.1016/j.asr.2016.04.031

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Summary:•A novel approach for reconfiguration of the satellite constellations is introduced.•Coupled non-simultaneous flight idea is presented to minimize reconfiguration phase.•Globally optimal solution is achieved by the efficient hybrid IWO/PSO technique. In this article, a novel approach is introduced for the satellite constellation reconfiguration based on Lambert’s theorem. Some critical problems are raised in reconfiguration phase, such as overall fuel cost minimization, collision avoidance between the satellites on the final orbital pattern, and necessary maneuvers for the satellites in order to be deployed in the desired position on the target constellation. To implement the reconfiguration phase of the satellite constellation arrangement at minimal cost, the hybrid Invasive Weed Optimization/Particle Swarm Optimization (IWO/PSO) algorithm is used to design sub-optimal transfer orbits for the satellites existing in the constellation. Also, the dynamic model of the problem will be modeled in such a way that, optimal assignment of the satellites to the initial and target orbits and optimal orbital transfer are combined in one step. Finally, we claim that our presented idea i.e. coupled non-simultaneous flight of satellites from the initial orbital pattern will lead to minimal cost. The obtained results show that by employing the presented method, the cost of reconfiguration process is reduced obviously.
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ISSN:0273-1177
1879-1948
DOI:10.1016/j.asr.2016.04.031