ISCAS OpenIR
Satellite Constellation Design for Complex Coverage
Ulybyshev Yuri
2008
SourceJournal of Spacecraft and Rockets
Volume45Issue:4Pages:843-849
English AbstractMost traditional satellite constellation design methods are associated with a simple zonal or global, continuous or discontinuous coverage connected with a visibility of points on the Earth's surface. A new geometric approach for more complex coverage of a geographic region is proposed. Full and partial coverage of regions is considered. It implies that, at any time, the region is completely or partially within the instantaneous access area of a satellite of the constellation. The key idea of the method is a two-dimensional space application for maps of the satellite constellation and coverage requirements. The space dimensions are right ascension of ascending node and argument of latitude. Visibility requirements of each region can be presented as a polygon and satellite constellation as a uniform moving grid. At any time, at least one grid vertex must belong to the polygon. The optimal configuration of the satellite constellation corresponds to the maximum sparse grid. The method is suitable for continuous and discontinuous coverage. In the last case, a vertex belonging to the polygon should be examined with a revisit time. Examples of continuous coverage for a space communication network and of the United States are considered. Examples of discontinuous coverage are also presented.
Indexed Type其他
Cooperation Status其它
Language英语
Content Type期刊论文
URIhttp://ir.iscas.ac.cn/handle/311060/1342
Collection中国科学院软件研究所
Recommended Citation
GB/T 7714
Ulybyshev Yuri. Satellite Constellation Design for Complex Coverage[J]. Journal of Spacecraft and Rockets,2008,45(4):843-849.
APA Ulybyshev Yuri.(2008).Satellite Constellation Design for Complex Coverage.Journal of Spacecraft and Rockets,45(4),843-849.
MLA Ulybyshev Yuri."Satellite Constellation Design for Complex Coverage".Journal of Spacecraft and Rockets 45.4(2008):843-849.
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