A self-calibration method for non-orthogonal angles of gimbals in rotational inertial navigation system based on fiber optic gyro

Rotating modulation technique is a mature method that has been widely used in the rotational inertial navigation system (RINS). Tri-axis RINS has three gimbals, and the Inertial Measurement Unit can rotate along three directions to modulate the inertial devices’ errors, so that the navigation accuracy of the system can be greatly improved. However, the outputs of attitudes are easily affected by the non-orthogonal angles of gimbals, which should be accurately calibrated and compensated. In this paper, the effects of the non-orthogonal angles on the attitudes are discussed detailed and simulations based on Matlab are conducted to verify that firstly; then, a self-calibration method based on the outputs of the fiber optic gyroscope and photoelectric encoder is proposed. Experimental results in a real tri-axis RINS show that the attitude outputs accuracy are improved from 150” to less than 10”, which verify the practicability of the calibration method proposed in this paper.

[1]  Songlai Han,et al.  An eight-position self-calibration method for a dual-axis rotational Inertial Navigation System , 2015 .

[2]  Bo Wang,et al.  Error modulation scheme analysis of dual-axis rotating strap-down inertial navigation system based on FOG , 2014, CCC 2014.

[3]  Bo Wang,et al.  A Self-Calibration Method for Nonorthogonal Angles Between Gimbals of Rotational Inertial Navigation System , 2015, IEEE Transactions on Industrial Electronics.

[4]  Qian Zhang,et al.  Innovative self-calibration method for accelerometer scale factor of the missile-borne RINS with fiber optic gyro. , 2016, Optics express.

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

[6]  Lei Wang,et al.  A rapid and high-precision initial alignment scheme for dual-axis rotational inertial navigation system , 2017 .

[7]  Qian Zhang,et al.  Analysis and Improvement of Attitude Output Accuracy in Rotation Inertial Navigation System , 2015 .

[8]  Kui Li,et al.  A Self-Calibration Method for Non-Orthogonal Angles of Gimbals in Tri-Axis Rotational Inertial Navigation System , 2016, IEEE Sensors Journal.

[9]  Rao Gu-yin,et al.  On the Theory of Optical Gyro Rotating Inertial Navigation System , 2006 .

[10]  Khalid Satori,et al.  A Self-Calibration Method of Zooming Camera , 2016, Int. J. Interact. Multim. Artif. Intell..

[11]  Huaxiang Cai,et al.  Iterative Learning Control with Extended State Observer for Telescope System , 2015 .

[12]  Chris Hide,et al.  Increased error observability of an inertial pedestrian navigation system by rotating IMU , 2014 .

[13]  Dan Liao,et al.  Error compensation of an optical gyro INS by multi-axis rotation , 2012 .

[14]  Chao Zhang,et al.  High precision locking control based on fiber optic gyro and photoelectric encoder for rotational inertial navigation system , 2016, IEICE Electron. Express.

[15]  Xingshu Wang,et al.  Optical Angular Encoder Installation Error Measurement and Calibration by Ring Laser Gyroscope , 2010, IEEE Transactions on Instrumentation and Measurement.

[16]  Yihua Yan,et al.  Calibration and data processing Chinese Spectral Radioheliograph , 2015 .

[17]  Chris Hide,et al.  Rotating a MEMS inertial Measurement Unit for a foot-mounted Pedestrian Navigation , 2014, J. Comput. Sci..

[18]  Fang Liu,et al.  Error analyses and calibration methods with accelerometers for optical angle encoders in rotational inertial navigation systems. , 2013, Applied optics.

[19]  Wang Lei,et al.  Calibration and data processing technology of gyroscope in dual axis rotational inertial navigation system , 2017 .