| タイトル | Control response measurements of the Skyship-500 airship |
| 著者（英） | Jex, H. R.; Gelhausen, P.; Hogue, J. R. |
| 著者所属（英） | Systems Technology, Inc.|NASA Ames Research Center |
| 発行日 | 1985-01-01 |
| 言語 | eng |
| 内容記述 | An examination is conducted of the Skyship 500's dynamic response to control inputs from elevators, rudders, and throttles at zero, 25, and 40 kts indicated airspeed. Input frequency sweeps were made with pitch and turn controls at 25 and 40 kts, ranging in frequency from about 0.03 to 1.5 Hz. FFT data analysis was then applied to compute describing functions for each run. Frequency responses are noted to be very smooth, and comparisons between repeat runs indicate excellent agreement. Summary plots of the faired describing functions from each run form the core of the data presented. These data constitute a comprehensive and reliable data base on which to predicate future dynamic simulation mathematical models of small airship dynamic response. |
| NASA分類 | AIRCRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 85A38796
AIAA PAPER 85-0881 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/390861 |
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