Q3504373: Difference between revisions
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Q3504373
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Latest revision as of 12:54, 2 September 2025
A fine guidance sensor (FGS) is an instrument on board a space telescope that provides high-precision pointing information as input to the telescope's attitude control systems. Interferometric FGSs have been deployed on the Hubble Space Telescope; a different technical approach is used for the James Webb Space Telescope's FGSs. In some specialized cases, such as astrometry, FGSs can also be used as scientific instruments.
Wikimedia, Wikidata
FGS
Ashkenaz, Calvinist Republic of Ghent, Chinland, Havilah, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, Dong Fang Hong 2, Ekran, Republic of Haiti, Fine Guidance Sensor, Fine guidance sensor,
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Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| class | space instrument | Fine Guidance Sensor | fine guidance sensor | Wikidata | |
| commons | image | Euclid’s Fine Guidance Sensor (FGS) is a completely new development in Europe, and it is responsible for ensuring the mission points with precision, performing all the ‘slews’ (rotations) that a six-year survey mission requires. | Commons | ||

