| タイトル | Stability and control flight test results of the space transportation system's orbiter |
| 著者（英） | Cooke, D. R.; Culp, M. A. |
| 著者所属（英） | NASA Johnson Space Center|McDonnell-Douglas Technical Services Co., Inc. |
| 発行日 | 1982-08-01 |
| 言語 | eng |
| 内容記述 | Flight testing of the Space Shuttle Orbiter is in progress and current results of the post-flight aerodynamic analyses are discussed. The purpose of these analyses is to reduce the pre-flight aerodynamic uncertainties, thereby leading to operational certification of the Orbiter flight envelope relative to the integrated airframe and flight control system. Primary data reduction is accomplished with a well documented maximum likelihood system identification techniques. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 82A40283
AIAA PAPER 82-1316 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/409517 |
