Abstract The OTV fulfills orbital maneuver by selecting appropriate transfer points to save fuels. Usually, before the orbital maneuver, it shall carry out non-powered free sliding in large elliptic orbit for a long time. During such process, due to the longer sliding period, the error of inertial navigation will be accumulated as time elapses. Meanwhile, when the orbit arrives at a certain height, the availability of satellite navigation signals becomes poor, the flight vehicle could not obtain accurate position and velocity with the INS/GNSS-integrated navigation in real time.


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    Titel :

    Orbit Prediction Technology


    Beteiligte:
    Li, Xuefeng (Autor:in) / Li, Chaobing (Autor:in)


    Erscheinungsdatum :

    01.01.2018


    Format / Umfang :

    14 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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