| タイトル | Development and testing of laser Doppler system components for wake vortex monitoring. Volume 1: Scanner development, laboratory and field testing and system modeling |
| 本文（外部サイト） | http://hdl.handle.net/2060/19740025837 |
| 著者（英） | Krause, M. C.; Morrison, L. K.; Shrider, K. R.; Jetton, J. L.; Coffey, E. W.; Huang, C. C.; Wilson, D. J.; Edwards, B. B. |
| 著者所属（英） | Lockheed Missiles and Space Co. |
| 発行日 | 1974-08-01 |
| 言語 | eng |
| 内容記述 | A servo-controlled range/elevation scanner for the laser Doppler velocimeter (LDV) was developed and tested in the field to assess its performance in detecting and monitoring aircraft trailing vortices in an airport environment. The elevation scanner provides a capability to manually point the LDV telescope at operator chosen angles from 3.2 deg. to 89.6 deg within 0.2 deg, or to automatically scan the units between operator chosen limits at operator chosen rates of 0.1 Hz to 0.5 Hz. The range scanner provides a capability to manually adjust the focal point of the system from a range of 32 meters to a range of 896 meters under operator control, or to scan between operator chosen limits and at rates from 0.1 Hz to 6.9 Hz. The scanner controls are designed to allow simulataneous range and elevation scanning so as to provide finger scan patterns, arc scan patterns, and vertical line scan patterns. The development and testing of the unit is discussed, along with a fluid dynamic model of the wake vortex developed in a laser Doppler vortex sensor simulation program. |
| NASA分類 | INSTRUMENTATION AND PHOTOGRAPHY |
| レポートNO | 74N33950
NASA-CR-120466
LMSC-HREC-TR-D390159-1 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/192825 |
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