| タイトル | Improved Correction System for Vibration Sensitive Inertial Angle of Attack Measurement Devices |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040086752 |
| 著者（英） | Finley, Tom D.; Crawford, Bradley L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2000-01-01 |
| 言語 | eng |
| 内容記述 | Inertial angle of attack (AoA) devices currently in use at NASA Langley Research Center (LaRC) are subject to inaccuracies due to centrifugal accelerations caused by model dynamics, also known as sting whip. Recent literature suggests that these errors can be as high as 0.25 deg. With the current AoA accuracy target at LaRC being 0.01 deg., there is a dire need for improvement. With other errors in the inertial system (temperature, rectification, resolution, etc.) having been reduced to acceptable levels, a system is currently being developed at LaRC to measure and correct for the sting-whip-induced errors. By using miniaturized piezoelectric accelerometers and magnetohydrodynamic rate sensors, not only can the total centrifugal acceleration be measured, but yaw and pitch dynamics in the tunnel can also be characterized. These corrections can be used to determine a tunnel's past performance and can also indicate where efforts need to be concentrated to reduce these dynamics. Included in this paper are data on individual sensors, laboratory testing techniques, package evaluation, and wind tunnel test results on a High Speed Research (HSR) model in the Langley 16-Foot Transonic Wind Tunnel. |
| NASA分類 | Research and Support Facilities (Air) |
| レポートNO | AIAA Paper 2000-0415 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/88592 |
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