The gyroscope, accelerometer and angular encoder are the most important components in a dual-axis rotation inertial navigation system (RINS). However, there are asynchronies among the sensors, which will thus lead to navigation errors. The impact of asynchrony between the gyroscope and angular encoder on the azimuth error and the impact of asynchrony between the gyroscope and accelerometer on the velocity error are analyzed in this paper. A self-calibration method based on navigation errors is proposed based on the analysis above. Experiments show that azimuth and velocity accuracy can be improved by compensating the asynchronies
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
To overcome the demerit that the calculation error of angular velocity is divergent with time in Gyr...
Rotation modulation is an effective method to enhance the accuracy of an inertial navigation system ...
Calibration and compensation techniques are essential to improve the accuracy of the strap-down iner...
The navigation accuracy of the inertial navigation system (INS) can be greatly improved when the ine...
The navigation accuracy of the inertial navigation system (INS) can be greatly improved when the ine...
When using modern navigation systems as part of an on-board system, the navigation task can be solve...
When using modern navigation systems as part of an on-board system, the navigation task can be solve...
The errors of inertial sensors affect the navigation accuracy of the strapdown inertial navigation s...
The Semi-Strapdown Inertial Navigation System (SSINS) provides a new solution to attitude measuremen...
The Semi-Strapdown Inertial Navigation System (SSINS) provides a new solution to attitude measuremen...
Inertial navigation system (INS) measures vehicle’s angular rate and acceleration by orthogonally mo...
In the dual-axis rotation inertial navigation system (INS), besides the gyro error, accelerometer er...
In the dual-axis rotation inertial navigation system (INS), besides the gyro error, accelerometer er...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
To overcome the demerit that the calculation error of angular velocity is divergent with time in Gyr...
Rotation modulation is an effective method to enhance the accuracy of an inertial navigation system ...
Calibration and compensation techniques are essential to improve the accuracy of the strap-down iner...
The navigation accuracy of the inertial navigation system (INS) can be greatly improved when the ine...
The navigation accuracy of the inertial navigation system (INS) can be greatly improved when the ine...
When using modern navigation systems as part of an on-board system, the navigation task can be solve...
When using modern navigation systems as part of an on-board system, the navigation task can be solve...
The errors of inertial sensors affect the navigation accuracy of the strapdown inertial navigation s...
The Semi-Strapdown Inertial Navigation System (SSINS) provides a new solution to attitude measuremen...
The Semi-Strapdown Inertial Navigation System (SSINS) provides a new solution to attitude measuremen...
Inertial navigation system (INS) measures vehicle’s angular rate and acceleration by orthogonally mo...
In the dual-axis rotation inertial navigation system (INS), besides the gyro error, accelerometer er...
In the dual-axis rotation inertial navigation system (INS), besides the gyro error, accelerometer er...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
We examine the feasibility of designing an accelerometer-based (or gyroscope-free) inertial navigati...
To overcome the demerit that the calculation error of angular velocity is divergent with time in Gyr...