Disclosed is a vertical flight path angle steering system for aircraft, utilizing a digital flight control computer which processes pilot control inputs and aircraft response parameters into suitable elevator commands and control information for display to the pilot on a cathode ray tube. The system yields desirable airplane control handling qualities and responses as well as improvements in pilot workload and safety during airplane operation in the terminal area and under windshear conditions.


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    Title :

    Vertical flight path steering system for aircraft


    Contributors:

    Publication date :

    1983-02-08


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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