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
Link To Document :
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