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Methodology development for evaluation of selective-fidelity rotorcraft simulationThis paper addressed the initial step toward the goal of establishing performance and handling qualities acceptance criteria for realtime rotorcraft simulators through a planned research effort to quantify the system capabilities of 'selective fidelity' simulators. Within this framework the simulator is then classified based on the required task. The simulator is evaluated by separating the various subsystems (visual, motion, etc.) and applying corresponding fidelity constants based on the specific task. This methodology not only provides an assessment technique, but also provides a technique to determine the required levels of subsystem fidelity for a specific task.
Document ID
19930021502
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Lewis, William D.
(NASA Ames Research Center Moffett Field, CA, United States)
Schrage, D. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Prasad, J. V. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Wolfe, Daniel
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Publication Information
Publication: NASA(FAA Helicopter Simulator Workshop
Subject Category
Research And Support Facilities (Air)
Accession Number
93N30691
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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