Abstract
In this study, dual-satellite lunar global navigation systems that consist of a constellation of two navigation satellites providing geo-spatial positioning on the lunar surface were compared. In our previous work, we proposed a new dual-satellite relative-positioning navigation method called multi-epoch double-differenced pseudorange observation (MDPO). While the mathematical model of the MDPO and its behavior under specific conditions were studied, we did not compare its performance with other dual-satellite relative-positioning navigation systems. In this paper, we performed a comparative analysis between the MDPO and other two dual-satellite navigation methods. Based on the difference in their mathematical models, as well as numerical simulation results, we developed useful insights on the system design of dual-satellite lunar global navigation systems.
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Tanaka, T., Ebinuma, T., Nakasuka, S., & Malki, H. (2021). A comparative analysis of multi-epoch double-differenced pseudorange observation and other dual-satellite lunar global navigation systems. Aerospace, 8(7). https://doi.org/10.3390/aerospace8070191
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