Satellite tends to be microminiaturization in the future. It needs to adopt a small, cheap and middle precision autonomous navigation system. According to the measurements of three-axis magnetometer in the body frame, the parameters of the orbit can be determined by using of Kalman Filter.The result of simulation shows that orbit determination by dint of three-axis magnetometer is of medium precision, which can satisfy some requirments of orbit determination.
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吴美平,田菁,胡小平.三轴磁强计轨道确定[J].国防科技大学学报,2002,24(3):90-93. WU Meiping, TIAN Jing, HU Xiaoping. Three-Axis Magnetometer Orbit Determination[J]. Journal of National University of Defense Technology,2002,24(3):90-93.