| タイトル | The Microwave Anisotropy Probe (MAP) Attitude Control System |
| 本文（外部サイト） | http://hdl.handle.net/2060/20020024132 |
| 著者（英） | Ward, David K.; ODonnell, James R., Jr.; Andrews, Stephen F.; Bauer, Frank H.; Ericsson, Aprille J.; Markley, F. Landis |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2002-01-01 |
| 言語 | eng |
| 内容記述 | The Microwave Anisotropy Probe mission is designed to produce a map of the cosmic microwave background radiation over the entire celestial sphere by executing a fast spin and a slow precession of its spin axis about the Sun line to obtain a highly interconnected set of measurements. The spacecraft attitude is sensed and controlled using an Inertial Reference Unit, two Autonomous Star Trackers, a Digital Sun Sensor, twelve Coarse Sun Sensors, three Reaction Wheel Assemblies, and a propulsion system. This paper describes the design of the attitude control system that carries out this mission and presents some early flight experience. |
| NASA分類 | Space Radiation |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/225417 |
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