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ROLM computers in the flight testing of the Fokker F29 aircraftThe design, development, installation, and operation of the test equipment (MRVS) is discussed. The main feature of the MRVS is continuous recording on an instrumentation recorder data of up to 1500 parameters with a total sample rate of up to 10,000 samples per second. In order to compress the evaluation and calibration time period, the following additional requirements were set for two test systems: (1) recording of selected parameters, time tagged on computer compatible tape (CCT); (2) recording of selected high bandwidth signals and ad hoc parameters on analog tape; (3) onboard presentation of calibrated parameter data, in engineering units, in numerical as well as graphical form for: system checkout during pre-, in- and post-flight, and quick look analysis during in-flight; (4) real time presentation on the ground by telemetry for: flight monitoring, takeoff and landing measurements, and noise measurements; and (5) data processing on the ground on the Fokker-NLR computer network.
Document ID
19820006966
Document Type
Conference Paper
Authors
Manders, P. J. (National Aerospace Lab. Amsterdam, Netherlands)
Date Acquired
August 10, 2013
Publication Date
December 1, 1981
Publication Information
Publication: NASA. Langley Research Center Ruggedized Minicomputer Hardware and Software Topics, 1981
Subject Category
COMPUTER SYSTEMS
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820006956Analytic PrimaryRuggedized minicomputer hardware and software topics, 1981: Proceedings of the 4th ROLM MIL-SPEC Computer User's Group Conference