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Simulation evaluation of two VTOL control/display systems in IMC approach and shipboard landingTwo control/display systems, which differed in overall complexity but were both designed for VTOL flight operations to and from small ships in instrument meteorological conditions (IMC), were tested using the Ames Flight Simulator for Advanced Aircraft (FSAA). Both systems have attitude command in transition and horizontal-velocity command in hover; the more complex system also has longitudinal-acceleration and flightpath-angle command in transition, and vertical-velocity command in hover. The most important overall distinction between the two systems for the viewpoint of implementation is that in one - the more complex - engine power and nozzle position are operated indirectly through flight controllers, whereas in the other they are operated directly by the pilot. Simulated landings were made on a moving model of a DD 963 Spruance-class destroyer. Acceptable transitions can be performed in turbulence of 3 m/sec rms using either system. Acceptable landings up to sea state 6 can be performed using the more complex system, and up to sea state 5 using the other system.
Document ID
19850006532
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 5, 2013
Publication Date
December 1, 1984
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-85996
A-9838
NAS 1.15:85996
Report Number: NASA-TM-85996
Report Number: A-9838
Report Number: NAS 1.15:85996
Accession Number
85N14841
Funding Number(s)
PROJECT: RTOP 505-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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