Design and Calibration of MIMU Based on Chip Size Micro Inertial Sensors

With rapid development of micro fabrication technology, the performance of MIMU has gradually improved. The MIMU introduced in this paper is based on the silicon micro machined gyroscope of type MSG7000D and accelerometer of type MSA6000. The volume of it is 3×3×3cm3, the mass is 68.5g and the power consumption is less than 1w. The experimental result shows that the bias stability of the gyroscope and accelerometer for each axis of the designed MIMU is less than 10°/h and 0.5mg respectively. For the non orthogonality in three axes of the structure, MIMU needs to be calibrated. After calibration, the measurement accuracy has improved by an order of magnitude. The designed MIMU can satisfy the requirement of high performance, low cost, light weight and small size for strap-down navigation system, thus it can be widely applied not only to the field of vehicles integrated navigation, attitude measurement but also to the fields of personal goods such as mobile, game consoles and so on.

[1]  Johann Borenstein,et al.  Precision calibration of fiber-optics gyroscopes for mobile robot navigation , 2000, Proceedings 2000 ICRA. Millennium Conference. IEEE International Conference on Robotics and Automation. Symposia Proceedings (Cat. No.00CH37065).

[2]  Naser El-Sheimy,et al.  A new multi-position calibration method for MEMS inertial navigation systems , 2007 .

[3]  Neil M Barbour,et al.  Inertial Navigation Sensors , 2010 .

[4]  Sangchul Lee,et al.  Test and error parameter estimation for MEMS — based low cost IMU calibration , 2011 .

[5]  Elham Vakil Asadollahei Miniature folded MEMS-IMU development toward implantable vestibular prosthesis , 2012 .

[6]  Jan Kenneth Bekkeng Calibration of a Novel MEMS Inertial Reference Unit , 2009, IEEE Transactions on Instrumentation and Measurement.

[7]  Louis Coryell,et al.  Low cost MEMS based INS for land-based military SATCOM OTM , 2012, MILCOM 2012 - 2012 IEEE Military Communications Conference.