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    Flight test of navigation and guidance sensor errors measured on STOL approaches (1979)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Navigation and guidance sensor error characteristics were measured during STOL approach-flight investigations. Data from some of the state sensors of a digital avionics system were compared to corresponding outputs from an inertial navigation system. These sensors include the vertical gyro, compass, and accelerometers. Barometric altimeter data were compared to altitude measured by a tracking radar. Data were recorded with the Augmentor Wing Jet STOL Research Aircraft parked and in flight.
    Keywords: AIRCRAFT INSTRUMENTATION
    Type: NASA-TM-81154 , A-8008
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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