A two segment approach configuration using inertially derived flight path angle to damp the glide path and upper segment approach paths is developed in the text. System performance in both head and tail winds is evaluated. Stability analysis is also presented on root locus plots for the capture and track modes. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Glide Path Augmentation with Inertial Flight Path Angle


    Contributors:
    V. Muehter (author)

    Publication date :

    1974


    Size :

    36 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Glide path indicator

    ATKINSON DAVID CHARLES | European Patent Office | 2018

    Free access

    GLIDE PATH INDICATOR

    ATKINSON DAVID CHARLES | European Patent Office | 2018

    Free access

    GLIDE PATH INDICATOR

    ATKINSON DAVID CHARLES | European Patent Office | 2015

    Free access

    GLIDE PATH INDICATOR

    ATKINSON DAVID CHARLES | European Patent Office | 2018

    Free access

    Glide path indicator

    ATKINSON DAVID CHARLES | European Patent Office | 2015

    Free access