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Two sets of linearized aircraft equations of motion for control system analysisDeveloping mathematical model for tandem rotor helicopter for analysis of automatic approach and landing system
Document ID
19710002750
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
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
August 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
PM-56
NASA-TM-X-66493
Report Number: PM-56
Report Number: NASA-TM-X-66493
Accession Number
71N12225
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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