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    Attitude determination and relative positioning for LEO satellites using arrays of GNSS sensors

    Access Status
    Fulltext not available
    Authors
    Nadarajah, Nandakumaran
    Teunissen, Peter
    Verhagen, S.
    Date
    2016
    Type
    Conference Paper
    
    Metadata
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    Citation
    Nadarajah, N. and Teunissen, P. and Verhagen, S. 2016. Attitude determination and relative positioning for LEO satellites using arrays of GNSS sensors, International Association of Geodesy Symposia, pp. 743-749.
    Source Title
    International Association of Geodesy Symposia
    DOI
    10.1007/1345_2015_26
    ISBN
    9783319246031
    School
    Department of Spatial Sciences
    URI
    http://hdl.handle.net/20.500.11937/15496
    Collection
    • Curtin Research Publications
    Abstract

    © Springer International Publishing Switzerland 2015. Global Navigation Satellite Systems (GNSS) have become ubiquitous in positioning, guidance and navigation. GNSS-based attitude determination and relative navigation are the important and promising applications. In this contribution we explore the potential of Low Earth Orbiting (LEO) satellite navigation in formation using arrays of GNSS sensors. We consider multiple LEO platforms in close formation, each equipped with multiple GNSS antennas/receivers. Platform processing involves precise attitude determination using the Multivariate Constrained Least-squares AM Biguity Decorrelation Adjustment (MCLAMBDA) method effectively utilizing known antenna geometry in local body frame. Between-platform processing involves estimation of unconstrained baselines between platforms using array-aided relative positioning effectively exploiting the platform antenna geometry in improving between-platform ambiguity resolution and baseline estimates. Finally, we use nonlinear recursive filtering to further improve the attitude angular estimates and between-platform baseline estimates. Our hardware-in-the-loop experiment with space enabled Namuru GNSS receivers shows the potential of stand-alone, unaided, single-frequency attitude determination and relative positioning of LEO satellites.

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