spase://CNES/Instrument/CDPP-AMDA/FREJA/MFE

The Swedish satellite, FREJA, was launched 6 October, 1992 into a 63 degree inclination, 600x1700 km altitude orbit.
The satellite is in the auroral zone a significant amount of the time. Ionospheric current systems are monitored by the Johns
Hopkins University Applied Physics Laboratory (JHU/APL) Magnetic Field Experiment (MFE). The MFE for the FREJA spacecraft was
provided as the only US principal experiment by the JHU/APL in cooperation with the NASA/Goddard Space Flight Center.

    The FREJA MFE includes a custom JHU/APL-designed Forth Reduced Instruction Set Computer (FRISC) microprocessor. The purpose of 
    the MFE computer is to allow extensive on board processing which has traditionally been performed after-the-fact on recorded data. 
    One of the many on board functions is an auroral zone field-aligned current detector patterned after the UARS MFE peak detector AC 
    channel. The 1.5 - 128 Hz bandpassed channel of the spin axis fluxgate magnetometer sensor is monitored by a one second standard 
    deviation calculation. When this result exceeds a programmable threshold (presently set at 100 nT) a trigger word is set which 
    circulates through the satellite telemetry system and can be used to initiate various experiment data taking. This MFE trigger value 
    is time-tagged, stored in the spacecraft housekeeping telemetry, and may be transmitted by an auxiliary, limited bandwidth transmitter 
    and received in near real time by a simple, portable antenna and receiver. The advantage of this detection approach is the simplicity 
    of the analysis and the direct, automatic and real time correlation with current systems previously determined by extensive ground 
    processing. This detector information can be received real-time or transferred via network or telephone from the receiving station 
    in Kiruna, Sweden using PC-based communications packages.