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Controlled impact demonstration flight data recorders/cockpit voice recordersIt was found that the sampling rates from flight recorders on a remotely piloted transport aircraft that crashed into the ground were too low, although they were higher than those required now by regulations. For example, the sampling rate for roll angle was one per second. The sampling rate for normal acceleration was also fairly low. Existing regulations require only 4 samples per second; researchers had 16 samples per second. Some data was lost during the initial impact. The frequency response data was adequate.
Document ID
19860012473
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Garodz, L. J.
(Federal Aviation Agency Atlantic City, NJ, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Publication Information
Publication: NASA. Langley Research Center Full-Scale Transport Controlled Impact Demonstration
Subject Category
Structural Mechanics
Accession Number
86N21944
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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