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The use of automatic control theory and a pilot math model in helicopter manual control system synthesisUsing automatic control theory with simple pilot model for synthesizing helicopter landing approach flight director control laws
Document ID
19710002749
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Collins, D. (NASA Electronics Research Center Cambridge, MA, United States)
Rempfer, P. S. (NASA Electronics Research Center Cambridge, MA, United States)
Stevenson, L. (NASA Electronics Research Center Cambridge, MA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
PM-64
NASA-TM-X-66492
Report Number: PM-64
Report Number: NASA-TM-X-66492
Accession Number
71N12224
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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