2019 9th International Conference on Recent Advances in Space Technologies (RAST) 2019
DOI: 10.1109/rast.2019.8767818
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Solar Sail Application with a Proposed Low Earth Orbit Mission Concept

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“…x 2 −p 2 dx. For the singularity of the upper limit of integration, since the orbital height of the LEO satellite is generally about 800 km [70], and the electron density is very rare above this height, the corresponding bending angle or dTEC is also close to 0, so the method of directly truncating the lower-limit singularity, a higher calculation accuracy can be expected. Currently, the occultation products officially provided by COSMIC and FY-3C adopt this method.…”
Section: Appendix a Data Preprocessingmentioning
confidence: 99%
“…x 2 −p 2 dx. For the singularity of the upper limit of integration, since the orbital height of the LEO satellite is generally about 800 km [70], and the electron density is very rare above this height, the corresponding bending angle or dTEC is also close to 0, so the method of directly truncating the lower-limit singularity, a higher calculation accuracy can be expected. Currently, the occultation products officially provided by COSMIC and FY-3C adopt this method.…”
Section: Appendix a Data Preprocessingmentioning
confidence: 99%