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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    Title :

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


    Contributors:

    Published in:

    Publication date :

    1979-11-01


    Size :

    694965 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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