Multi-position self-calibration method of inertial navigation system
In order to solve the problem that in the dual axle rotating modulation inertial navigation system the angle between the horizon roller of the system and horizontal plane cant be removed,this paper provides an on-line self calibration method based on inertial navigation system,and this method realized the on-line self calibration of the inertial navigation system by calculating bias and scale factor both of the gyroscope and accelerometer,solving the problem that in the dual axle rotating modulation inertial navigation system the angle between the horizon roller of the system and horizontal plane cant be removed,providing an calculable basis for the prediction of attitude angle and realizing on-line autonomous self-calibration.
on-line self calibration inertial navigation system (INS) bias scale factor azimuth axis pitching axis horizontal roller
Jiwei Zhang Xiaodong Xu Bo Wang
School of Automation, Beijing Institute of Technology, China
国际会议
太原
英文
146-150
2012-08-17(万方平台首次上网日期,不代表论文的发表时间)