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  • 1970-1974  (2)
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  • 1
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-27
    Description: Attitude controllers are used to guide roll, pitch, and yaw of vehicle in flight. Controllers enclose multitude of switches, gears, cams, and other hardware needed to transmit pilot's commands to attitude control systems. New design, using magnetic coupled transducers, eliminates many mechanical parts, improving reliability and reducing maintenance.
    Keywords: MECHANICS
    Type: MSC-12394
    Format: application/pdf
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  • 2
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-27
    Description: The reported flight controller features a handle grip which is mounted on a longitudinally extending control element. The handle grip is pivotally mounted on the control element about a pitch axis which is perpendicular to the longitudinal axis through the control element. The pivotal mounting includes a resilient force mounting mechanism which centers the grip relative to the control element. Rotation of the handle grip produces a direct rotation of a transducer element in a transducer which provides an electrical indication of the rotative movement about three mutually perpendicular axes.
    Keywords: COMPUTERS
    Format: application/pdf
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