Acquisition of the Flight Information Using the KSR-3 Agnetometer

Details Acquisition of the Flight Information Using the KSR-3 Agnetometer Acquisition of the Flight Information Using the KSR-3 Agnetometer

Mar 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003jass...20...29k&link_type=abstract

Journal of Astronomy and Space Sciences. Vol. 20, no. 1, p.29-42

Astronomy and Astrophysics

Astronomy

Magnetometer, Fluxgate, Flight Attitude

Scientific paper

The KSR-3 magnetometers consist of the fluxgate magnetometer (MAG/AIM) for acquiring the rocket flight attitude information, and the search-coil magnetometer (MAG/SIM) for the observation of the Earth's magnetic fluctuations. The position (latitude, longitude, and height) and flight condition (the transformation angle) of the rocket is measured after the data based on these two magnetometers are compared with IGRF. The gap in the vector of magnetic field between the position of the launching point and an impact point is taken into account in data reduction. Angular variation of pitch, yaw, and roll can be researched when the data is applied to the coordinate system of the rocket.

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