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. [1]
The Hubble Space Telescope has three fine guidance sensors (FGSs). Two are used to point and lock the telescope onto the target, and the third can be used for position measurements – also known as astrometry. Because the FGSs are so accurate, they can be used to measure stellar distances and also to investigate binary star systems.
The three FGSs are located at 90-degree intervals around the circumference of the telescope's field of view. To achieve the very high pointing accuracy Hubble needs, the FGSs have been constructed as interferometers to exploit the wavelike features of the in-coming starlight. With this kind of accuracy and precision, the sensors can search for a wobble in the motion of nearby stars that could indicate the presence of a planetary companion, determine if certain stars really are double stars, measure the angular diameter of stars, galaxies, etc.
Due to the sensitivity of the FGS they can not be used whilst the HST is pointed within 50 degrees of the Sun.
A guiding system, also called FGS, but using different technology is used for the James Webb Space Telescope (JWST). It provides input for the observatory's attitude control system (ACS). During on-orbit commissioning of the JWST, the FGS also provided pointing error signals during activities to achieve alignment and phasing of the segments of the deployable primary mirror. [3]
The JWST FGS, designed and built by COM DEV International, was supplied by the Canadian Space Agency. To save on mass and volume it was assembled into a single unit together with the Near Infrared Imager and Slitless Spectrograph, but they are separate optical instruments.
The JWST FGS-Guider has three main functions. The first is to obtain images for target acquisition. Full-frame images are used to identify star fields by correlating the observed brightness and position of sources with the properties of catalogued objects selected by the observation planning software. The second is to acquire pre-selected guide stars. During acquisition, a guide star is first centred in an 8 × 8 pixel window. Small angle maneuvers are then executed to translate this window to a pre-specified location within the field of view, so that an observation with one of the science instruments will be oriented correctly. The third function is to provide the ACS with centroid measurements of the guide stars at a rate of 16 times per second. These measurements will be used to enable stable pointing at the milliarcsecond level.
The FGS will be sensitive enough to reach 58 μJy at 1.25 μm (~Jab = 19.5), and has a 2.4×2.4 arcminute square field of view. This combination of sky coverage and sensitivity ensures that an appropriate guide star can be found with 95% probability at any point in the sky, including high galactic latitudes.
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Fine Guidance Sensor and Near Infrared Imager and Slitless Spectrograph (FGS-NIRISS) is an instrument on the James Webb Space Telescope (JWST) that combines a Fine Guidance Sensor and a science instrument, a near-infrared imager and a spectrograph. The FGS/NIRISS was designed by the Canadian Space Agency (CSA) and built by Honeywell as part of an international project to build a large infrared space telescope with the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA). FGS-NIRISS observes light from the wavelengths of 0.8 to 5.0 microns. The instrument has four different observing modes.
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Fine Guidance Sensor (FGS) for the Hubble Space Telescope is a system of three instruments used for pointing the telescope in space, and also for astrometry and its related sciences. To enable aiming the telescope at a specific spot in the sky, each FGS combines optics and electronics. There are three Hubble FGS, and they have been upgraded over the lifetime of the telescope by crewed Space Shuttle missions. The instruments can support pointing of 2 milli-arc seconds. The three FGS are part of the Hubble Space Telescope's Pointing Control System, aka PCS. The FGS function in combination with the Hubble main computer and gyroscopes, with the FGS providing data to the computer as sensors which enables the HST to track astronomical targets.
María Begoña Vila Costas is a Spanish astrophysicist specializing in the study of spiral galaxies. She currently resides in Washington, D.C. and works as a systems engineer at NASA's Goddard Space Flight Center. She is the lead engineer for the Fine Guidance Sensor and Near Infrared Imager and Slitless Spectrograph (FGS-NIRISS) on the James Webb Space Telescope – the Hubble's successor – in addition to being in charge of the final cold test of the group of instruments before their integration with the telescope. She is now working on the Nancy Grace Roman Space Telescope.
The James Webb Space Telescope (JWST) is a space telescope designed primarily to conduct infrared astronomy. Its complex launch and commissioning process lasted from late 2021 until mid-2022.