• → European Space Agency

      • Space for Europe
      • Space News
      • Space in Images
      • Space in Videos
    • About Us

      • Welcome to ESA
      • DG's News and Views
      • For Member State Delegations
      • Business with ESA
      • ESA Exhibitions
      • ESA Publications
      • Careers at ESA
    • Our Activities

      • Space News
      • Observing the Earth
      • Human Spaceflight
      • Launchers
      • Navigation
      • Space Science
      • Space Engineering
      • Operations
      • Technology
      • Telecommunications & Integrated Applications
    • For Public

    • For Media

    • For Educators

    • For Kids

    • ESA

    • Observing the Earth

    • Living Planet

    • Meteorological missions

    • MetOp

    • MetOp at a glance
    • Overview
    • Why we need MetOp
    • Facts & figures
    • History
    • Satellite

      • About the satellite
      • Payload Module
      • Service Module
    • Instruments

      • Overview
      • Technical summary
    • Launch

      • Launch sequence
      • Launcher
    • Mission operations

      • Operations
      • Orbit
    • Resources

      • Publications
      • General links
      • Glossary
      • Acronym list
    • Multimedia
    • MetOp images
    • MetOp videos
    • MetOp animations
    • Help
    • Services
    • Subscribe

    ESA > Our Activities > Observing the Earth > The Living Planet Programme > Meteorological missions > MetOp

    GOME-2 scan unit

    The Scan Unit (SU) contains a rotating mirror, situated optically in front of the spectrometer, and its related mechanics and electronics. To perform global Earth coverage, GOME-2's instantaneous on-ground field of view has to be scanned in the across-track direction. The field of view may be varied in size from 320 km x 40 km to 960 km x 80 km.

    The SU is physically subdivided into two assemblies: the Mechanical Assembly (SUMA) and the Electronics Assembly (SUEA). The SUMA is almost identical to that of GOME-1, with a rotating mirror installed on an axis actuated by a brushless three-phase motor. A major improvement with respect to the GOME-1 design is the presence of a wireless angular-position resolver; which removes all electrical connections between fixed and rotating parts, leading to a notable reliability gain.

    Another positive consequence of such a design is the possibility to perform continuous (360°) rotations of the Scan Mirror at a speed of 10 rpm. This feature, exercised every now and then, will allow redistribution of the lubricant that could accumulate in some parts of the bearing races due to wear, so recovering the original smoothness and precision of movement. Another minor improvement is better confinement of the debris generated by the bearing wear itself.

    The SUEA is a separate box, which contains all of the electronics needed for closed-loop control of the scan mirror angular position. It is able to implement five scan profiles at constant angular speed (as per GOME-1) and five new scans, compensating for the Earth's curvature and providing a constant linear scan speed on the ground. A new wide-amplitude scan corresponding to 1920 km on the ground is also implemented, which will allow complete Earth coverage in 1.5 days. All scans are completely in-flight reprogrammable, allowing an almost unlimited choice of profiles. The basic scan timing is 4.5 sec for the forward scan and 1.5 sec for the flyback.

    The mirror movements are synchronised with the global instrument timings (detector integration times, and so on). In the event of a failure in the synchronisation interfaces, the Scan Unit can autonomously perform a pre-programmed series of operations, in order to partially recover the mission. The Unit's overall performance remains the same as for GOME-1; mirror positioning accuracy in fixed pointing will be better than 0.03° (corresponding to about 800 m on the ground), while in scanning modes it will depend on actual speed, but will anyway be better than 0.065°.

    Last update: 28 June 2006

    Rate this

    Views

    Share

    • Currently 0 out of 5 Stars.
    • 1
    • 2
    • 3
    • 4
    • 5
    Rating: 0/5 (0 votes cast)

    Thank you for rating!

    You have already rated this page, you can only rate it once!

    Your rating has been changed, thanks for rating!

    40
    Tweet
    • In depth
    • About GOME-2
    • Description
    • Spectrometer
    • Polarisation
    • Calibration unit
    • Focal-plane assemblies
    • Scan unit
    • Control and data handling system
    • Performance
    • Products
    • Calibration/validation
    • Ground processor Prototype
    • Related articles
      • Monitoring ozone with GOME-2
      • MetOp's instruments
      • A/DCS
      • AMSU-A1
      • AMSU-A2
      • ASCAT
      • AVHRR
      • GOME-2
      • GRAS
      • HIRS
      • IASI
      • MHS
      • SARP-3
      • SARR
      • SEM

    Connect with us

    • RSS
    • Youtube
    • Twitter
    • Flickr
    • G+
    • Facebook
    • Livestream
    • Subscribe
    • App Store
    • LATEST ARTICLES
    • · ESA astronaut Timothy Peake set fo…
    • · Space drives e-mobility
    • · Proba-V opens its eyes
    • · First new Galileo satellite arrive…
    • · Next destination: space
    • FAQ

    • Jobs at ESA

    • Site Map

    • Contacts

    • Terms and conditions