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Algorithm for Simulating Atmospheric Turbulence and Aeroelastic Effects on Simulator Motion SystemsAtmospheric turbulence produces high frequency accelerations in aircraft, typically greater than the response to pilot input. Motion system equipped flight simulators must present cues representative of the aircraft response to turbulence in order to maintain the integrity of the simulation. Currently, turbulence motion cueing produced by flight simulator motion systems has been less than satisfactory because the turbulence profiles have been attenuated by the motion cueing algorithms. This report presents a new turbulence motion cueing algorithm, referred to as the augmented turbulence channel. Like the previous turbulence algorithms, the output of the channel only augments the vertical degree of freedom of motion. This algorithm employs a parallel aircraft model and an optional high bandwidth cueing filter. Simulation of aeroelastic effects is also an area where frequency content must be preserved by the cueing algorithm. The current aeroelastic implementation uses a similar secondary channel that supplements the primary motion cue. Two studies were conducted using the NASA Langley Visual Motion Simulator and Cockpit Motion Facility to evaluate the effect of the turbulence channel and aeroelastic model on pilot control input. Results indicate that the pilot is better correlated with the aircraft response, when the augmented channel is in place.
Document ID
20120014294
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Ercole, Anthony V.
(State Univ. of New York Binghamton, NY, United States)
Cardullo, Frank M.
(State Univ. of New York Binghamton, NY, United States)
Kelly, Lon C.
(Unisys Corp. Hampton, VA, United States)
Houck, Jacob A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 26, 2013
Publication Date
August 1, 2012
Subject Category
Man/System Technology And Life Support
Report/Patent Number
L-20173
NF1676L-15219
NASA/TM-2012-217601
Funding Number(s)
WBS: WBS 160961.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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