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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    Title :

    Orbit Prediction Technology


    Contributors:
    Li, Xuefeng (author) / Li, Chaobing (author)


    Publication date :

    2018-01-01


    Size :

    14 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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