Radar attitude sensing system for use in earth orbital and lunar orbital vehicles is described; this multi-purpose flight control instrument employs radar data to obtain vehicle roll, pitch, yaw, altitude and velocity; it uses light weight radar with electronically steered antenna to provide all solid state sensor with no moving parts; system employs monopulse antenna configuration; operation is described at block diagram level; theoretical performance is determined and is compared with results from aircraft flight test program; these results are extrapolated to orbital altitudes and velocities; test results show good comparison with predicted performance. (38487)


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    Titel :

    Radar attitude sensing system


    Weitere Titelangaben:

    IEEE Conv Rec


    Beteiligte:
    Burcher, E. (Autor:in) / Rupp, E. (Autor:in)

    Kongress:

    IEEE Electronic and Aerospace Systems Convention -- EASCON '68 ; 1968 ; United States , Washington, DC


    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Radar attitude sensing system.

    Burcher, E. / Rupp, E. | NTRS | 1968




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