Optical Navigation Satellite Constellation Design

Jun Ao; Yi Wu; Chun Bo Ma

doi:10.4028/www.scientific.net/AMR.424-425.1065

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 424-425Optical Navigation Satellite Constellation Design

Optical Navigation Satellite Constellation Design

Abstract:

Satellite constellation has incomparable superiority compared to the single satellite, and can provide effective global intermittent or continuous coverage. This paper designs a laser navigation satellite constellation by simulating the coverage properties of single satellite. The running track of the satellite constellation covers the specified area and provides intermittent navigation information for mobile platforms.

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Periodical:

Advanced Materials Research (Volumes 424-425)

Pages:

1065-1069

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.424-425.1065

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Online since:

January 2012

Authors:

Jun Ao, Yi Wu, Chun Bo Ma

Keywords:

Coverage, Optical Navigation, Satellite Constellation, Simulation

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References

[1] L. Olivier, N. Richard, C. Mathieu, Enhancing the economics of communications satellites via orbital reconfigurations and staged deployment, AIAA 2003 – 6317 (2003).

DOI: 10.2514/6.2003-6317

Google Scholar

[2] J. Munson, C. Jilla, An optimization approach to the launch vehicle selection process for satellite constellations. AIAA 2000 - 1122 (2000).

DOI: 10.2514/6.2000-1122

Google Scholar

[3] Y. Zhang, Y. Zhang, Calculation of subsatellite track of remote sensing satellite in nearly round orbit, Journal of Institute of Surveying and Mapping, Vol. 18, No. 4, pp : 257-259.

Google Scholar

[4] J.J. Wang and W. Zhang, Design of Formation Flying Satellites's Initial Parameters and Perturbation Analysis, A Erospace Shanghai, No. 2: 30-35, (2008).

Google Scholar

[5] Y. Liu, A. Yu, and J. Zhu, A Measurement Fusion Algorithm for Orbit Paramenters Estimation of Formation Flying Satellites, Journal of Electronic & Information Technology, Vol. 29, No. 11: 2679-2682, (2007).

Google Scholar

[6] H. Wang, L. Chen, and X. Ren, Simulation Analysis and Optimization of Constellation's Global Continuous Coverage, Chinese Space Science and Technology, No. 1, pp: 16-22, (2001).

Google Scholar