Optical system, designed to monitor attitude of missile during early launch phase, uses passive reflective components mounted on missile to return pair of laser beams transmitted from ground station; beams have their polarization state modulated by reflective elements such that polarization is function of missile attitude; returned beams are passed through polarization analyzing system at ground station and missile attitude computed from measured polarization parameters.


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    Titel :

    Missile attitude sensing with polarized laser beams


    Weitere Titelangaben:

    Canaveral Council Tech Soc -- Space Congress


    Beteiligte:
    Dailey, J.L. (Autor:in)

    Kongress:

    2nd Proceedings of Canaveral Council Technical Society -- Space Congress ; 1965 Control



    Erscheinungsdatum :

    1965


    Format / Umfang :

    18 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Technique for remote sensing of missile position and attitude (Technical rept.)

    Conard, R.G. / Pell, K.M. / Nyda, J.E. | Tema Archiv | 1975


    Status of the Laser Automated Missile Position and Attitude Measurement System

    K. Pell / A. Presson / R. Conard et al. | NTIS | 1977



    Measurement of Missile Position and Attitude by Lasers

    R. G. Conard / K. M. Pell / J. E. Nydahl | NTIS | 1975