| The inertial navigation systems are generally formed by gyroscopes and accelerometers. Gyroscopes are used for measuring the angular motion parameters and accelerometers for the linear acceleration. The application technology of MEMS IMU has been widely thought much of. At present, the gyroscope free micro inertial measurement unit (GF-IMU) is one of the important research direction, because of the simple principle of the accelerometer the more potential to improve the performance of the accelerometer than that of the gyro. The specific force and angular rate are simultaneously calculated by outputs of the accelerometers forming the GF-SIMU. Using linear accelerometers instead of gyroscope in GF-SIMU not only can make the inertial navigation system cost, but also overcome the demerit of which gyroscope is incapable of the great angle motion and the strong shock. In this paper, the main research work is on the method of installation error parameter calibration and compensation of GF-SIMU.Fistly, the work is how to calculate the angular velocity from the accelerometer outputs in GF-SIMU. The way to calculate the angular velocity is subject to the positions and sensitive directions of the accelerometers. Furthermore, under a new six accelerometers configuration mode, it is derived theoretically and simulated for the method on calculating angular velocity and acceleration; And it is derived theoretically and simulated for the method on calculating angular velocity and acceleration under the installation of position error and the installation azimuth error. Last, the angular rate is analyzed in the case of installation error which brings the larger calculating error. According to this, a new calculating method, that is called "first position, last azimuth", is proposed in this paper. And it is used to get the estimated equation of accelerometer output, and then get exacter angular velocity. |
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