袁林, 吴长水. Research on Low-accuracy IMU and GPS Combined Navigation System[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(4): 573-580.
DOI:
袁林, 吴长水. Research on Low-accuracy IMU and GPS Combined Navigation System[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(4): 573-580. DOI: 10.13433/j.cnki.1003-8728.20230151.
Research on Low-accuracy IMU and GPS Combined Navigation System
To improve the accuracy and precision of automatic navigation system for agricultural machinery
this paper designs an intelligent combined navigation system for agricultural machinery based on Global Positioning System (GPS) and Inertial Navigation System (INS) for the problems of relatively large measurement error of low-accuracy Inertial Measurement Unit (IMU) and nonlinearity of the filtering model. The system takes the low-accuracy IMU/GPS tight combination model as the framework
the system state equation and measurement equation are derived
the extended Kalman filter(EKF) algorithm is used to correct the error of INS with real-time feedback
and finally a real-vehicle test platform to verify the automatic navigation system is built under low-speed scenarios. The test results show that the tight combination system proposed in this paper reduces the longitude
latitude
northward velocity
and eastward velocity errors (standard deviation) by 24%
47%
50% and 54% respectively
which proves that the tight combination can effectively suppress the navigation error dispersion
compared with the loose combination system; and the EKF also effectively improves the navigation accuracy and enhances the filtering effect compared with the Kalman filter (KF) algorithm.