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YF-12 cooperative airframe/propulsion control system program, volume 1Several YF-12C airplane analog control systems were converted to a digital system. Included were the air data computer, autopilot, inlet control system, and autothrottle systems. This conversion was performed to allow assessment of digital technology applications to supersonic cruise aircraft. The digital system was composed of a digital computer and specialized interface unit. A large scale mathematical simulation of the airplane was used for integration testing and software checkout.
Document ID
19810004533
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, D. L.
(Lockheed-California Co. Burbank, CA, United States)
Connolly, G. F.
(Lockheed-California Co. Burbank, CA, United States)
Mauro, F. M.
(Lockheed-California Co. Burbank, CA, United States)
Reukauf, P. J.
(Lockheed-California Co. Burbank, CA, United States)
Marks, R.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1136
NASA-CR-163099
SP-5317
Report Number: H-1136
Report Number: NASA-CR-163099
Report Number: SP-5317
Accession Number
81N13044
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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