The highly maneuverable aircraft technology (HiMAT) program was conceived to demonstrate advanced technology concepts through scaled-aircraft flight tests using a remotely piloted technique. Closed-loop primary flight control is performed from a ground-based cockpit, utilizing a digital computer and up/down telemetry links. A backup flight control system for emergency operation resides in an onboard computer. The onboard systems are designed to provide fail-operational capabilities and utilize two microcomputers, dual uplink receiver/decoders, and redundant hydraulic actuation and power systems. This paper discusses the design and validation of the primary and backup digital flight control systems as well as the unique pilot and specialized systems interfaces.


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    Title :

    Flight control systems development of highly maneuverable aircraft technology /HiMAT/ vehicle


    Contributors:

    Conference:

    American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting ; 1979 ; New York, NY


    Publication date :

    1979-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English