| タイトル | Modeling Reaction Control System Effects on Mars Odyssey |
| 本文（外部サイト） | http://hdl.handle.net/2060/20020076394 |
| 著者（英） | Wilmoth, Richard G.; Hanna, Jill L.; Chavis, Zachary Q.; Bushnell, Dennis M. |
| 著者所属（英） | NASA Langley Research Center|Institute for Computer Applications in Science and Engineering |
| 発行日 | 2002-07-01 |
| 言語 | eng |
| 内容記述 | During the Mars 2001 Odyssey aerobraking mission, NASA Langley Research Center performed 6 degree of freedom (6-DOF) simulations to determine rotational motion of the spacecraft. The main objective of this study was to assess the reaction control system models and their effects on the atmospheric flight of Odyssey. Based on these models, a comparison was made between data derived from flight measurements to simulated rotational motion of the spacecraft during aerobraking at Mars. The differences between the simulation and flight derived Odyssey data were then used to adjust the aerodynamic parameters to achieve a better correlation. |
| NASA分類 | Numerical Analysis |
| レポートNO | ICASE-2002-31
NAS 1.26:211767
NASA/CR-2002-211767 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/91230 |
