发明名称 ROTATION ANGLE MEASURING CONTROL METHOD FOR ROTATING MISSILE, AND ROTATING MISSILE
摘要 PROBLEM TO BE SOLVED: To obtain a reference azimuth signal using voltage waveform generated with geomagnetism as the magnetic field from a coil in a missile flying while rotating. SOLUTION: In this rotation angle measuring control method for the rotating missile, the missile 1 provided with the coil c is discharged, and the reference azimuth signal which is a rotation angle in space of the missile 1 is obtained from the voltage waveform generated with geomagnetism as the magnetic field from the coil c in the missile rotating around a center axis as the rotational center. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2006098010(A) 申请公布日期 2006.04.13
申请号 JP20040286645 申请日期 2004.09.30
申请人 TAMAGAWA SEIKI CO LTD 发明人 SUGIURA TSUNEO
分类号 F42B10/26;F42B10/66;F42B15/01;G01B7/30 主分类号 F42B10/26
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