LRBET4 program best-estimated-of-trajectory (BET) calculation for post-flight trajectory analysis of Shuttle orbiter. Produces estimated measurements for comparing predicted and actual trajectory of Earth-orbiting spacecraft. Kalman filter and smoothing filter applied to input data to estimate state vector, reduce noise, and produce BET. LRBET4 written in FORTRAN IV for batch execution.


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    Title :

    Analyzing Shuttle Orbiter Trajectories


    Contributors:
    Lear, W. M. (author)

    Published in:

    Publication date :

    1986-05-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Shuttle orbiter vibroacoustics

    Colonna, R. A. / Mccutchen, D. K. / Allen, H. C. et al. | NTRS | 1979


    Space Shuttle Orbiter Barricade

    P. R. Digiovanniantonio | NTIS | 1974



    Space shuttle orbiter avionics

    Carrier, L.M. / Minor, R.G. | Tema Archive | 1977