Quick calibration method for inertial measurement unit

摘要

The invention relates to a quick calibration method for an inertial measurement unit (IMU). According to the method, a user holds and rotates the IMU to move in all directions without any external equipment, so that twelve error coefficients including gyro biases, gyro scale factors, accelerometer biases and accelerometer scale factors can be accurately calibrated in a short time. The quick calibration method for the IMU is characterized by being free of hardware cost, high in efficiency and simple and easy to implement, and can ensure certain calibration precision. Thus, the quick calibration method is especially suitable for in-situ quick calibration for the medium- and low-grade IMUs, thereby effectively solving the problem of environmental sensitivity of the error coefficients of the mechanical IMU, and promoting popularization and application of MEMS (micro-electro mechanical systems) inertial devices.

主权项

1. A quick calibration method for an inertial measurement unit (IMU), characterized in comprising the following steps that:
Step 1) after an inertial measurement system is warmed up, whether an initial horizontal attitude angle of the IMU is known is determined; if yes, moving to Step 3; and if no, moving to Step 2; Step 2) the IMU is maintained in a static state for a period and the initial horizontal attitude angle of the IMU is calculated approximately according to measurement information of an accelerometer and a gyro during the period; Step 3) an initial heading angle of the IMU is set at random; and Step 4) the IMU is rotated around a measurement center thereof, and to-be-estimated gyro and accelerometer error coefficients are calculated based on the known initial horizontal attitude angle or the initial horizontal attitude angle obtained in Step 2 and the initial heading angle obtained in Step 3, wherein during calculation, position variation and velocity variation of the IMU are both set as zero, and respectively represent pseudo-position observation information and pseudo-velocity observation information.