| タイトル | Angle of attack system |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830010498 |
| 著者（英） | Finley, T. D. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1983-03-01 |
| 言語 | eng |
| 内容記述 | The development of systems for measuring model pitch and roll attitude in the National Transonic Facility (NTF) is discussed. The effort is divided between two approaches: (1) an inertial measurement that is an extrapolation of existing technology into a cryogenic environment, and (2) an optical technique based on a holographic angle sensor. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 83N18769 |
| 権利 | No Copyright |
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