Satellite Constellation Orbit Design Optimization with Combined Genetic Algorithm and Semianalytical Approach

This paper focuses on maximizing the percent coverage and minimizing the revisit time for a small satellite constellation with limited coverage. A target area represented by a polygon defined by grid points is chosen instead of using a target point only. The constellation consists of nonsymmetric an...

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Bibliographic Details
Main Authors: Tania Savitri, Youngjoo Kim, Sujang Jo, Hyochoong Bang
Format: Article
Language:English
Published: Hindawi Limited 2017-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2017/1235692