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Fidelity Assessment Of A Uh 60a Simulation On The Nasa Ames Vertical Motion Simulator
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723580147 Total Pages :324 pages Book Rating :4.5/5 (81 download)
Book Synopsis Fidelity Assessment of a Uh-60a Simulation on the NASA Ames Vertical Motion Simulator by : National Aeronautics and Space Administration (NASA)
Download or read book Fidelity Assessment of a Uh-60a Simulation on the NASA Ames Vertical Motion Simulator written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 324 pages. Available in PDF, EPUB and Kindle. Book excerpt: Helicopter handling qualities research requires that a ground-based simulation be a high-fidelity representation of the actual helicopter, especially over the frequency range of the investigation. This experiment was performed to assess the current capability to simulate the UH-60A Black Hawk helicopter on the Vertical Motion Simulator (VMS) at NASA Ames, to develop a methodology for assessing the fidelity of a simulation, and to find the causes for lack of fidelity. The approach used was to compare the simulation to the flight vehicle for a series of tasks performed in flight and in the simulator. The results show that subjective handling qualities ratings from flight to simulator overlap, and the mathematical model matches the UH-60A helicopter very well over the range of frequencies critical to handling qualities evaluation. Pilot comments, however, indicate a need for improvement in the perceptual fidelity of the simulation in the areas of motion and visual cuing. The methodology used to make the fidelity assessment proved useful in showing differences in pilot work load and strategy, but additional work is needed to refine objective methods for determining causes of lack of fidelity. Atencio, Adolph, Jr. Ames Research Center NASA-TM-104016, A-93071, NAS 1.15:104016, USAATC-TR-93-A-005, AD-A271172 RTOP 505-59-52...
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