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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Simulating the Liaison Navigation Concept in a Geo + Earth-Moon Halo Constellation


    Contributors:

    Conference:

    International Symposium on Space Flight Dynamics ; 2012 ; Pasadena, CA, United States


    Publication date :

    2012-10-29


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Liaison Navigation in the Sun-Earth-Moon Four-Body Problem (AAS 06-221)

    Hill, K. / Lo, M. W. / Born, G. H. et al. | British Library Conference Proceedings | 2006



    Transfers to Earth-Moon L3 Halo Orbits

    Davis, Kathryn / Born, George / Deilami, Masoud et al. | AIAA | 2012


    Transfers to Earth–Moon L3 halo orbits

    Davis, Kathryn | Online Contents | 2013


    Low Earth orbit constellation design using the Earth-Moon L1 point

    Kasdin, N. J. / Gralla, Erica / Chow, Naomi | NTRS | 2004