DocumentCode :
2113813
Title :
A Three Axis Magnetometer For use in a Small Satellite
Author :
Richard, Ing Linhart
Author_Institution :
Pilsen Univ., Pilsen
fYear :
2006
fDate :
6-7 Sept. 2006
Firstpage :
113
Lastpage :
116
Abstract :
This paper deals with a construction of a three axis magnetometer for use in a small satellite. It is necessary to know the magnetic field around the satellite for an attitude stabilisation and for propulsion. A minimal weight, size and power consumption are the most critical properties of this construction. The magnetic flux has to be measured in an 8-bit resolution. Two small packages with magnetoriesistive sensors from HONEYWELL are used. One package measures magnetic flux in the axis X and Y, and second in the axis Z. The microcontroller is used for data processing, sensors setup and for communication over central bus. Other units in the satellite are able to read the results of the magnetic field measurement over this bus. The software in the microcontroller has to remove any noise and electrical offsets from the data, improves the immunity to an impulse disturbances and a magnetic offsets caused by other electric circuits in the satellite. Construction of this magnetometer is one part of a large project, whose aim is to build Czech amateur satellite compatible with the CubeSat technology.
Keywords :
aerospace computing; aerospace instrumentation; aerospace propulsion; artificial satellites; attitude control; magnetic field measurement; magnetometers; magnetoresistance; microcontrollers; attitude stabilisation; magnetic field measurement; magnetoriesistive sensors; microcontroller; propulsion; small satellite; three axis magnetometer; Data processing; Energy consumption; Magnetic field measurement; Magnetic flux; Magnetic sensors; Magnetometers; Microcontrollers; Packaging; Propulsion; Satellites;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Applied Electronics, 2006. AE 2006. International Conference on
Conference_Location :
Pilsen
Print_ISBN :
80-7043-442-2
Type :
conf
DOI :
10.1109/AE.2006.4382978
Filename :
4382978
Link To Document :
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