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  • A Xylophone Bar Magnetometer for micro/pico satellites

    Paper number

    IAC-09.C2.8.1

    Author

    Dr. Véronique Rochus, University of Liege, Belgium

    Coauthor

    Dr. Véronique Rochus, University of Liege, Belgium

    Coauthor

    Dr. Hervé Lamy, Royal Observatory of Belgium, Belgium

    Coauthor

    Mr. Innocent Niyonzima, University of Liege, Belgium

    Coauthor

    Prof. Pierre Rochus, Centre Spatial de Liège, Belgium

    Year

    2009

    Abstract
    Magnetic fields play a key role in many aspects of the solar-terrestrial interactions. For example, during geomagnetic activity, charged particles precipitate along geomagnetic field lines and produce spectacular aurora.  Strong sheets of field-aligned currents (FACs) associated with these precipitations produce local perturbations of the geomagnetic field.  A magnetometer onboard a spacecraft (s/c) crossing these current sheets will record the magnetic field perturbations from which the values of the FACs can be deduced from Maxwell’s equation rot(B) = μ0 J.  With a single s/c this relies on the assumption that the current sheet is stationary during the crossing. However this assumption is not always valid which means that spatial and temporal variations of the magnetic field cannot be discriminated.  Currently the separation of satellites in multi-s/c missions like Cluster or Themis is larger than the width of the current sheet.  This is one example where multi-point measurements are needed with a fleet of small micro- or pico-s/c with smaller separations.
    
    The Belgian Institute of Space Aeronomy (BIRA-IASB), the “Centre Spatial de Liège” (CSL), the “Laboratoire de Techniques Aéronautiques et Spatiales” (LTAS) of University of Liège, and the Microwave Laboratory of University of Louvain-La-Neuve are collaborating in order to develop a miniature version of a xylophone bar magnetometer (XBM) with Micro-Electro-Mechanical Systems (MEMS). The device is based on a classical resonating xylophone bar.  A sinusoidal current is supplied to the bar oscillating at the fundamental transverse resonant mode of the bar. When there is an external magnetic field, the resulting Lorentz force causes the bar to vibrate at its fundamental frequency with amplitude directly proportional to the component of the ambient magnetic field perpendicular to the bar.  We will illustrate the working principles of the XBM and the challenges to reach the required sensitivity (measuring magnetic fields lower than ~ 10 nT). The optimal dimensions of the MEMS XBM will be discussed as well as the constraints on the current that can flow through the bar. Preliminary measurements and temperature and pressure effects on the device will be discussed based on a prototype that will be built in the Microwave Laboratory of University of Louvain-La-Neuve using Silicon on Insulator (SOI) technology.  Another important aspect to qualify this magnetometer for space applications is related to the minituarisation of the sensor that will measure the bar displacement and of the associated electronics. Several possible sensors will be discussed including capacitive methods, plasmons, etc … 
    
    
    Abstract document

    IAC-09.C2.8.1.pdf

    Manuscript document

    IAC-09.C2.8.1.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.