A digital autopilot design was developed for a small laser-guidedtactical missile. The multiloop design was developed in the w plane and analyzed by time domain simulation. Performance is as good or better than the current analog version, thus demonstrationg the feasibility of digital guidance technology in tactical missile applications.


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    Titel :

    Digital Autopilot Design for a Microprocessor-Controlled Small Tactical Terminal Homing Missile


    Beteiligte:
    Albanes, W.V. (Autor:in) / Bosley, J. T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.11.1979


    Format / Umfang :

    694965 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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