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Fixed-base simulation study of decoupled controls during approach and landing of a STOL transport airplaneA fixed-base visual simulation study has been conducted to evaluate the use of decoupled controls as a means for reducing pilot workload during approach and landing of an externally blown jet-flap short take-off and landing (STOL) transport. All six rigid-body degrees of freedom were employed with the aerodynamic characteristics based on wind-tunnel data. The primary piloting task was to use a flight director to capture and maintain a two-segment glide slope, with a closed-circuit television display of a STOL airport used during simulations of the flare and landing. The decoupled longitudinal controls used constant prefilter and feedback gains to provide steady-state decoupling of flight-path angle, pitch angle, and forward velocity. The pilots were enthusiastic about the decoupled longitudinal controls but believed the decoupled concept offered no significant advantage over conventional controls in the lateral mode.
Document ID
19740007590
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Miller, G. K., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Deal, P. L.
(NASA Langley Research Center Hampton, VA, United States)
Champine, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
L-8825
NASA-TN-D-7363
Report Number: L-8825
Report Number: NASA-TN-D-7363
Accession Number
74N15703
Funding Number(s)
PROJECT: RTOP 501-26-05-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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