• DocumentCode
    2066598
  • Title

    Maximum likelihood estimation of navigation parameters from downlink telemetry

  • Author

    Vilnrotter, V. ; Andrews, K. ; Hamkins, J. ; Tkacenko, A.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    Deep-space navigation uses estimates of range and Doppler to update and improve spacecraft trajectory solutions. Operationally, Doppler is generally extracted directly from the ground receiver´s carrier tracking loop, and range is determined primarily by the use of specially designed ¿ranging tones,¿ or more recently (e.g., on New Horizons), Pseudo-Noise (PN) sequences. Transmission of tones or PN sequences drain power and bandwidth that could be better used for transmitting additional science data from the spacecraft. Here we describe and evaluate a novel technique that extracts range and Doppler estimates directly from the decoded data, thus enabling data-transmission at the maximum rate consistent with spacecraft range, antenna gain and available signal power. In this paper, the structure of the maximum likelihood estimator for range and Doppler is derived, and its performance determined relative to Crame¿r-Rao bounds via simulation and analysis. Performance of conventional Doppler and delay estimators based on carrier tracking loops is also derived, and contrasted with the performance of the optimum Doppler-delay estimator over a range of symbol SNR typically encountered in deep-space applications.
  • Keywords
    maximum likelihood estimation; pseudonoise codes; space communication links; space telemetry; space vehicles; Crame¿r-Rao bounds; Doppler estimation; antenna gain; carrier tracking loops; data transmission; deep-space navigation; downlink telemetry; maximum likelihood estimation; navigation parameters; pseudo-noise sequences; range estimation; ranging tones; spacecraft trajectory solution; Bandwidth; Data mining; Delay estimation; Downlink; Maximum likelihood decoding; Maximum likelihood estimation; Navigation; Space vehicles; Telemetry; Tracking loops;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2010 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-3887-7
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2010.5446954
  • Filename
    5446954