原文传递
Frequency-response techniques for documentation and improvement of rotorcraft simulators
| 题名： | Frequency-response techniques for documentation and improvement of rotorcraft simulators |
| 作者： | Tischler, Mark B. |
| 关键词： | documentation；simulator；improve；rotor；resp；craft；mathematical；characteristics；natural；research |
| 摘要： | Pilot-in-the-loop characterizations are most naturally formulated in terms of end-to-end frequency responses, so a frequency-response-based method is the natural approach to assessing simulator dynamic fidelity. A comprehensive frequency-response approach used heavily by Ames Research Center researchers was described, and results were presented from a number of simulator fidelity assessment studies. Those studies included UH-60 mathematical model validation and upgrade, ASTOVL linear model extraction, and documentation of the Vertical Motion Simulator (at Ames Research Center) motion and visual system characteristics. |
| 报告类型： | 科技报告 |
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