Abstract Navigation is the technology to provide navigation parameters for the motional carrier to arrive at the destination accurately from the starting point. During the flight process of the OTV, the basic navigation parameters needed are the orbital and attitude parameters. Among which, the orbital parameters refer to the position and velocity of the flight vehicle in navigation coordinate system (the selected reference coordinate system, for example, geocentric inertial coordinate system, launching inertial coordinate system and launching coordinate system). Attitude parameters refer to the position relations of carrier coordinate system of flight vehicle corresponding to the navigation coordinate system, usually described by three Eulerian angles of pitch, yaw, and rolling.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Inertial Navigation and Initial Alignment Technology


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


    Publication date :

    2018-01-01


    Size :

    15 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English






    Suboptimal filter algorithm of initial alignment in inertial navigation system

    Danli, W. / Hongyue, Z. / Gubarenco, S. I. | British Library Online Contents | 1999


    Research on Swaying Base Initial Alignment of Strapdown Inertial Navigation System

    Liu, Haiyang / Xu, Junhui / Zhen, Zhanchang | IEEE | 2018


    Independent initial alignment of marine strapdown inertial navigation system in moorage

    Zhou, L.-x. / Cui, Z.-x. | British Library Online Contents | 2002