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Digital autopilots: Design considerations and simulator evaluationsThe development of a digital autopilot program for a transport aircraft and the evaluation of that system's performance on a transport aircraft simulator is discussed. The digital autopilot includes three axis attitude stabilization, automatic throttle control and flight path guidance functions with emphasis on the mode progression from descent into the terminal area through automatic landing. The study effort involved a sequence of tasks starting with the definition of detailed system block diagrams of control laws followed by a flow charting and programming phase and concluding with performance verification using the transport aircraft simulation. The autopilot control laws were programmed in FORTRAN 4 in order to isolate the design process from requirements peculiar to an individual computer.
Document ID
19720004293
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Osder, S.
(Sperry Flight Systems Div. Moffett Field, CA, United States)
Neuman, F.
(NASA Ames Research Center Moffett Field, CA, United States)
Foster, J.
(NASA Ames Research Center)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Subject Category
Aircraft
Report/Patent Number
PUB-70-1364-00-00
NASA-TM-X-62094
Report Number: PUB-70-1364-00-00
Report Number: NASA-TM-X-62094
Accession Number
72N11942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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