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Relationship Between Optimal Gain and Coherence Zone in Flight SimulationIn motion simulation the inertial information generated by the motion platform is most of the times different from the visual information in the simulator displays. This occurs due to the physical limits of the motion platform. However, for small motions that are within the physical limits of the motion platform, one-to-one motion, i.e. visual information equal to inertial information, is possible. It has been shown in previous studies that one-to-one motion is often judged as too strong, causing researchers to lower the inertial amplitude. When trying to measure the optimal inertial gain for a visual amplitude, we found a zone of optimal gains instead of a single value. Such result seems related with the coherence zones that have been measured in flight simulation studies. However, the optimal gain results were never directly related with the coherence zones. In this study we investigated whether the optimal gain measurements are the same as the coherence zone measurements. We also try to infer if the results obtained from the two measurements can be used to differentiate between simulators with different configurations. An experiment was conducted at the NASA Langley Research Center which used both the Cockpit Motion Facility and the Visual Motion Simulator. The results show that the inertial gains obtained with the optimal gain are different than the ones obtained with the coherence zone measurements. The optimal gain is within the coherence zone.The point of mean optimal gain was lower and further away from the one-to-one line than the point of mean coherence. The zone width obtained for the coherence zone measurements was dependent on the visual amplitude and frequency. For the optimal gain, the zone width remained constant when the visual amplitude and frequency were varied. We found no effect of the simulator configuration in both the coherence zone and optimal gain measurements.
Document ID
20110014640
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Gracio, Bruno Jorge Correia
(Delft Univ. of Technology Delft, Netherlands)
Pais, Ana Rita Valente
(Delft Univ. of Technology Delft, Netherlands)
vanPaassen, M. M.
(Delft Univ. of Technology Delft, Netherlands)
Mulder, Max
(Delft Univ. of Technology Delft, Netherlands)
Kely, Lon C.
(NASA Langley Research Center Hampton, VA, United States)
Houck, Jacob A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
August 8, 2011
Subject Category
Aeronautics (General)
Report/Patent Number
1069480
NF1676L-12036
Meeting Information
Meeting: AIAA Modeling and Simulation Technologies Conference
Location: Portland, OR
Country: United States
Start Date: August 8, 2011
End Date: August 11, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 160961.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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