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  • Satellite flight dynamics activities supported by optical observations, lessons learnt from operational experience

    Paper number

    IAC-19,B6,1,7,x49204

    Author

    Ms. Noelia Sánchez-Ortiz, Spain, Deimos Space S.L.

    Coauthor

    Mr. Stefano Pessina, Germany, EUMETSAT

    Coauthor

    Mr. Raúl Domínguez-González, Spain, Deimos Space S.L.

    Coauthor

    Mr. Jaime Nomen, Spain, Deimos Space SLU

    Year

    2019

    Abstract
    Since June 2018 Eumetsat has incorporated optical observations into the operational orbit determination process for the 4 geosynchronous satellites METEOSAT, with the objective of assessing the suitability of optical data to support the operational orbit determination, and determining the accuracy of routine orbit determination and manoeuvres calibration using mixed data from ranging stations and telescopes.  Up to now, flight dynamic activities were based on ranging data from a network of stations, with alternate tracking from 2 stations per satellite. 
    
    The optical measurements are provided currently by the Deimos Sky Survey (DeSS) telescopes, using additional sensors as a backup in case of adverse weather conditions or technical issues. The processing of the measurement data is being performed by two separate teams at Eumetsat and Deimos. 
    
    Each satellite is observed at least twice per week, in routine mode, plus additional observations when required, for manoeuvre calibration purposes. The orbit determination based on those observations is automatically performed weekly by means of a Batch Least Squares approach with a two-week rolling window. In absence of manoeuvres, this allows determining the solar radiation pressure coefficient while maintaining consistency with the previously computed orbits. When a manoeuvre is scheduled, optical observations are taken as soon as possible after the manoeuvre itself. In this case, the paper shows that the orbit determination with optical information provides results comparable with the nominal range-only orbits, with accuracy gain in case of fusion of the different measurements.
    
    This paper describes the processing chain put in place at Deimos for scheduling and performing the observations, and for the processing of measurement data, and it summarizes the findings after nearly one year of service. The paper presents an evaluation of orbital quality and capability to estimate manoeuvres executed by the satellites, and identifies the benefits for satellite operators when using this novel approach for satellite operations based on this kind of observations.
    Abstract document

    IAC-19,B6,1,7,x49204.brief.pdf

    Manuscript document

    IAC-19,B6,1,7,x49204.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.