• The Programmable Dynamic Geomagnetic Field Simulator for Research of Satellite Operating on the Orbit ( The Satellite Test Facility on the Ground )


    Constitution：
    -three-axis Helmholtz coil system
    -programmable current source with double direction of
    output.
    -turning table without magnetism
    - magnetometers for monitoring magnetic field inside of
    coil system
    - computer for control of the system operating
    - one set of software for opening and closed operating.
    Function：
    - for measuring remnant magnetic moment of device
    and complete satellite
    - for determination of satellite’s interference to
    magnetometer 0nboard
    - for simulating effect of magnetic interference force
    moment on satellite attitude while its operating on the
    orbit
    - for scale and correction of magnetometer and
    magnetic torquer
    - for physical simulation of measuring by magnetometer
    & controlling by magnetic torquer small satellite
    attitude