Attitude sensor for spacecraft
1. Field of the Invention A spacecraft is provided that includes a communications payload having an antenna support structure and an antenna boom coupled to the antenna support structure. An attitude sensor may be mounted to the antenna boom. The attitude sensor (such as an Earth sensor, a star trac...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | 1. Field of the Invention
A spacecraft is provided that includes a communications payload having an antenna support structure and an antenna boom coupled to the antenna support structure. An attitude sensor may be mounted to the antenna boom. The attitude sensor (such as an Earth sensor, a star tracker and/or a sun sensor) may be mounted at a root of the antenna boom. |
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