Linked Autonomous Interplanetary Satellite Orbit Navigation, or LiAISON, is a novel satellite navigation technique where relative radiometric measurements between two or more spacecraft in a constellation are processed to obtain the absolute state of all spacecraft. The method leverages the asymmetry of the gravity field that the constellation exists in. This paper takes a step forward in developing a high fidelity navigation simulation for the LiAISON concept in an Earth-Moon constellation. In particular, we aim to process two-way Doppler measurements between a satellite in GEO orbit and another in a halo orbit about the Earth-Moon L1 point.
Simulating the Liaison Navigation Concept in a Geo + Earth-Moon Halo Constellation
International Symposium on Space Flight Dynamics ; 2012 ; Pasadena, CA, United States
2012-10-29
Conference paper
No indication
English
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