Application of Latitude Stripe Division in Satellite Constellation Coverage to Ground

Grid point technique is a classical method in computing satellite constellation coverage to the ground regions. Aiming at improving the low computational efficiency of the conventional method, a method using latitude stripe division is proposed, which has high efficiency, and we name it latitude str...

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Main Authors: Maocai Wang, Xin Luo, Guangming Dai, Xiaoyu Chen
Format: Article
Language:English
Published: Hindawi Limited 2016-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2016/4315026
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spelling doaj-b4efdbc83a4943669449f375ac7fb8b12020-11-24T22:47:53ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742016-01-01201610.1155/2016/43150264315026Application of Latitude Stripe Division in Satellite Constellation Coverage to GroundMaocai Wang0Xin Luo1Guangming Dai2Xiaoyu Chen3School of Computer, China University of Geosciences, Wuhan 430074, ChinaSchool of Computer, China University of Geosciences, Wuhan 430074, ChinaSchool of Computer, China University of Geosciences, Wuhan 430074, ChinaSchool of Computer, China University of Geosciences, Wuhan 430074, ChinaGrid point technique is a classical method in computing satellite constellation coverage to the ground regions. Aiming at improving the low computational efficiency of the conventional method, a method using latitude stripe division is proposed, which has high efficiency, and we name it latitude stripe method. After dividing the target region into several latitude stripes, the coverage status of each latitude stripe is computed by means of the spherical geometry relationship in the first orbital period. The longitude coverage intervals in the remaining orbital periods are computed by sliding the coverage status in the first orbital period. Based on this method, the instantaneous and cumulative coverage in simulation time can be calculated more efficiently. As well, the relationship between the cumulative coverage and altitude can be computed fast by this method, which could be used in the optimized design of repeating sun-synchronous orbits. The comparison between the conventional grid point method and the latitude stripe method shows that the latitude stripe method has high efficiency and accuracy. Through various case studies, the optimization in repeating sun-synchronous orbits design is successfully represented.http://dx.doi.org/10.1155/2016/4315026
collection DOAJ
language English
format Article
sources DOAJ
author Maocai Wang
Xin Luo
Guangming Dai
Xiaoyu Chen
spellingShingle Maocai Wang
Xin Luo
Guangming Dai
Xiaoyu Chen
Application of Latitude Stripe Division in Satellite Constellation Coverage to Ground
International Journal of Aerospace Engineering
author_facet Maocai Wang
Xin Luo
Guangming Dai
Xiaoyu Chen
author_sort Maocai Wang
title Application of Latitude Stripe Division in Satellite Constellation Coverage to Ground
title_short Application of Latitude Stripe Division in Satellite Constellation Coverage to Ground
title_full Application of Latitude Stripe Division in Satellite Constellation Coverage to Ground
title_fullStr Application of Latitude Stripe Division in Satellite Constellation Coverage to Ground
title_full_unstemmed Application of Latitude Stripe Division in Satellite Constellation Coverage to Ground
title_sort application of latitude stripe division in satellite constellation coverage to ground
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5966
1687-5974
publishDate 2016-01-01
description Grid point technique is a classical method in computing satellite constellation coverage to the ground regions. Aiming at improving the low computational efficiency of the conventional method, a method using latitude stripe division is proposed, which has high efficiency, and we name it latitude stripe method. After dividing the target region into several latitude stripes, the coverage status of each latitude stripe is computed by means of the spherical geometry relationship in the first orbital period. The longitude coverage intervals in the remaining orbital periods are computed by sliding the coverage status in the first orbital period. Based on this method, the instantaneous and cumulative coverage in simulation time can be calculated more efficiently. As well, the relationship between the cumulative coverage and altitude can be computed fast by this method, which could be used in the optimized design of repeating sun-synchronous orbits. The comparison between the conventional grid point method and the latitude stripe method shows that the latitude stripe method has high efficiency and accuracy. Through various case studies, the optimization in repeating sun-synchronous orbits design is successfully represented.
url http://dx.doi.org/10.1155/2016/4315026
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AT xinluo applicationoflatitudestripedivisioninsatelliteconstellationcoveragetoground
AT guangmingdai applicationoflatitudestripedivisioninsatelliteconstellationcoveragetoground
AT xiaoyuchen applicationoflatitudestripedivisioninsatelliteconstellationcoveragetoground
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