| タイトル | In flight estimations of Cassini spacecraft inertia tensor and thruster magnitude |
| 著者（英） | Lee, Allan Y.; Feldman, Antonette |
| 発行日 | 2006-05-01 |
| 言語 | eng |
| 内容記述 | This paper describes two methods used by the Cassini Attitude Control team to determine these key parameters and how flight telemetry was used to estimate them. The method for estimating the spacecraft inertia tensor exploits the conservation of angular momentum during spacecraft slews under reaction wheel control. |
| NASA分類 | Spacecraft Propulsion and Power |
| 権利 | Copyright |
