英文摘要 |
Due to the rapid development in semiconductor technology, MEMS (microelectromechanical system)-based sensors have been widely used in commercial and military applications. These sensors are characterized by their small size, low cost, low power consumption. However, MEMS sensors are noted for their low accuracy, limiting the applicability in high precision navigation and control. NSPO self-developed MEMS IRU (inertial reference unit) adopts a gyroscope cluster (16 3-axis gyroscopes) approach and optimal data fusion method to account for the limitation of MEMS sensors in terms of accuracy and reliability. Since the temperature variation affects the MEMS-based output in a nonlinear manner, a calibration curve was built into the processing model through offline data analysis. NSPO team has completed MEMS IRU Engineering Qualification Model (EOM). Moreover, the MEMS IRU, which can be integrated with NSPO self-developed multi gyro-stelar Inertial Attitude Estimate (IAE) to meet the requirement of the high accuracy remote sensing satellite mission. |