发明名称 Mitigation of drift effects in secondary inertial measurements of an isolated detector assembly
摘要 The 6-axis position and attitude of an imaging vehicle's detector assembly is measured by mounting the detector assembly on a compliant isolator and separating the main 6-axis IMU on the vehicle from a secondary IMU comprising at least inertial rate sensors for pitch and yaw on the detector assembly. The compliant isolator couples low-frequency rigid body motion of the vehicle below a resonant frequency to the isolated detector assembly while isolating the detector assembly from high-frequency attitude noise above the resonant frequency. A computer processes measurements of the 6-axis rigid body motion and the angular rate of change in yaw and pitch of the isolated detector assembly to mitigate the drift and noise error effects of the secondary inertial rate sensors and estimate the 6-axis position and attitude of the detector assembly.
申请公布号 US8552350(B2) 申请公布日期 2013.10.08
申请号 US201213350787 申请日期 2012.01.15
申请人 BIELAS MICHAEL S.;SCHLATTER EDWARD C.;FACCIANO ANDREW B.;THERIAULT PHILIP C.;EBEL JAMES A.;LAPORTE ROBERT J.;RAYTHEON COMPANY 发明人 BIELAS MICHAEL S.;SCHLATTER EDWARD C.;FACCIANO ANDREW B.;THERIAULT PHILIP C.;EBEL JAMES A.;LAPORTE ROBERT J.
分类号 F41G7/22;F41G7/00;F42B15/00;F42B15/01;G01S13/00;G01S13/89 主分类号 F41G7/22
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