Feasibility of GNSS in Cis-Lunar Space Spacecraft Autonomous Navigation
Abstract The feasibility of GNSS in cis-lunar space is simulated and analyzed from three aspects based on the classical cis-lunar orbit and circumlunar orbit: number of visible satellites, PDOP value, and dynamic characteristics. The results show that it is appropriate to set the carrier-to-noise ratio threshold of the receiver on the cis-lunar orbit and circumlunar orbit to 12 dB-Hz. Based on this analysis, we propose the technical issues of using GNSS signals in cis-lunar space spacecraft.
Key words :
GNSS
cis-lunar space
navigation
orbit determination
Cite this article:
WU Wei,LIU Huicui,CAO Jianfeng et al. Feasibility of GNSS in Cis-Lunar Space Spacecraft Autonomous Navigation[J]. jgg, 2023, 43(8): 795-800.
WU Wei,LIU Huicui,CAO Jianfeng et al. Feasibility of GNSS in Cis-Lunar Space Spacecraft Autonomous Navigation[J]. jgg, 2023, 43(8): 795-800.
URL:
http://www.jgg09.com/EN/ OR http://www.jgg09.com/EN/Y2023/V43/I8/795
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