An algorithm of state estimation with attitude motion for the powered flight phase by apogee boost motor of a geostationary satellite is presented. The measured Doppler data oscillate with a spin period for the satellite equipped with an offset antenna, or fluctuate due to the occurrence of apogee motor firing error. A technique for specification of the error resource against the orbit injection error is outlined. The estimation results by the simplified filter with attitude motion are discussed. The technique is especially suited to real time estimation during maneuvers with a liquid propellant motor.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    State Estimation Algorithm Considering Attitude Motion for Apogee Motor Burning of Geostationary Satellite


    Beteiligte:
    S. Ono (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    State estimation for solid apogee motor burning of geostationary satellite

    Ono, Shuji / Tomomura, Kiyoshi / Toyoda, Toshihiro | Elsevier | 1988



    Attitude motion compensation for imager on Fengyun-4 geostationary meteorological satellite

    Lyu, Wang / Dai, Shoulun / Dong, Yaohai et al. | Elsevier | 2017


    Apogee Boost Motor

    P. Strada | NTIS | 1989


    An apogee boost motor for the Geos European satellite

    GRANDE, G. / SCOLASTICO, U. | AIAA | 1975