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Simulation study of two VTOL control/display systems in IMC approach and landingBoth systems had full attitude command; the more complex system (Type 1) also had translational velocity command. The systems were applied to existing models of a VTOL lift-fan transport and the AV-8A Harrier. Simulated landings were made on a model of a DD963 Spruance-class destroyer. It was concluded that acceptable transitions and vertical landings can be performed, using the Type 1 system, in free-air turbulence up to 2.5 m/sec and sea state 6 and, using the Type 2 system, in free-air turbulence up to 1.5 m/sec and sea state 4.
Document ID
19810021598
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Merrick, V. K.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1981
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-81295
A-8592
Report Number: NASA-TM-81295
Report Number: A-8592
Accession Number
81N30136
Funding Number(s)
PROJECT: RTOP 505-42-71
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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