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Propulsion/flight control integration technology (PROFIT) software system definitionThe Propulsion Flight Control Integration Technology (PROFIT) program is designed to develop a flying testbed dedicated to controls research. The control software for PROFIT is defined. Maximum flexibility, needed for long term use of the flight facility, is achieved through a modular design. The Host program, processes inputs from the telemetry uplink, aircraft central computer, cockpit computer control and plant sensors to form an input data base for use by the control algorithms. The control algorithms, programmed as application modules, process the input data to generate an output data base. The Host program formats the data for output to the telemetry downlink, the cockpit computer control, and the control effectors. Two applications modules are defined - the bill of materials F-100 engine control and the bill of materials F-15 inlet control.
Document ID
19780021159
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carlin, C. M.
(Boeing Aerospace Co. Seattle, WA, United States)
Hastings, W. J.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-144876
Report Number: NASA-CR-144876
Accession Number
78N29102
Funding Number(s)
CONTRACT_GRANT: NAS4-2391
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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