发明名称 METHOD FOR CALIBRATING AN INERTIAL NAVIGATION SYSTEMWITH A LIMITED MECHANICAL TURNING RANGE
摘要 A method of calibrating an inertial unit having an inertial core with vibratory axisymmetric gyros, the method includes the steps of starting from a first position, causing the inertial core to pivot towards a second position about a pivot axis that is different from the sensing axes of the gyros and from a trisector thereof, while taking measurements of an angular orientation of the vibration of each gyro, the angular orientation being left free during pivoting; returning the inertial core to the first position; adjusting the angular orientation of the vibration of each gyro to a value corresponding to the second position; causing the inertial core to pivot towards the second position while once more taking measurements of the angular orientation of each gyro; and calibrating the inertial core as a function of the measurements taken.
申请公布号 EP2926088(A1) 申请公布日期 2015.10.07
申请号 EP20130795733 申请日期 2013.11.22
申请人 SAGEM DÉFENSE SÉCURITÉ 发明人 SALAÜN, ERWAN
分类号 G01C19/56;G01C25/00 主分类号 G01C19/56
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