NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Simulation System Fidelity Assessment at the Vertical Motion SimulatorFidelity is a word that is often used but rarely understood when talking about groundbased simulation. Assessing the cueing fidelity of a ground based flight simulator requires a comparison to actual flight data either directly or indirectly. Two experiments were conducted at the Vertical Motion Simulator using the GenHel UH-60A Black Hawk helicopter math model that was directly compared to flight data. Prior to the experiment the simulator s motion and visual system frequency responses were measured, the aircraft math model was adjusted to account for the simulator motion system delays, and the motion system gains and washouts were tuned for the individual tasks. The tuned motion system fidelity was then assessed against the modified Sinacori criteria. The first experiments showed similar handling qualities ratings (HQRs) to actual flight for a bob-up and sidestep maneuvers. The second experiment showed equivalent HQRs between flight and simulation for the ADS33 slalom maneuver for the two pilot participants. The ADS33 vertical maneuver HQRs were mixed with one pilot rating the flight and simulation the same while the second pilot rated the simulation worse. In addition to recording HQRs on the second experiment, an experimental Simulation Fidelity Rating (SFR) scale developed by the University of Liverpool was tested for applicability to engineering simulators. A discussion of the SFR scale for use on the Vertical Motion Simulator is included in this paper.
Document ID
20130014431
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Beard, Steven D.
(NASA Ames Research Center Moffett Field, CA, United States)
Reardon, Scott E.
(Science Applications International Corp. Moffett Field, CA, United States)
Tobias, Eric L.
(San Jose State Univ. Research Foundation San Jose, CA, United States)
Aponso, Bimal L.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 27, 2013
Publication Date
May 21, 2013
Subject Category
Air Transportation And Safety
Report/Patent Number
ARC-E-DAA-TN6410
Meeting Information
Meeting: American Helicopter Society (AHS) Annual Forum and Technology Display
Location: Phoenix, AZ
Country: United States
Start Date: May 21, 2013
End Date: May 23, 2013
Sponsors: American Helicopter Society, Inc.
Funding Number(s)
CONTRACT_GRANT: NNX08AI34A
CONTRACT_GRANT: NNA05BE28C
WBS: WBS 160961.02.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available