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An Accurate Calibration Method Based on Velocity in a Rotational Inertial Navigation System
Qian Zhang1, Lei Wang2, Zengjun Liu3
1School of Instrument Science and Opto-Electronics Engineering, Beihang University, Beijing 100191, China. victoryqian175@163.com.
This study introduces a new dual-axis rotation strategy for inertial navigation systems (INS), significantly reducing azimuth angle errors. A novel calibration method also improves velocity precision in rotational INS (RINS).
Area of Science:
- Navigation Systems
- Control Theory
- Sensor Fusion
Background:
- Inertial Navigation Systems (INS) accuracy is limited by sensor drifts and biases.
- Traditional rotational INS (RINS) modulates errors along a single axis, leaving some errors unaddressed.
- Azimuth angle error is particularly sensitive to vertical gyro drift, necessitating effective modulation.
Purpose of the Study:
- To propose a novel dual-axis rotation strategy for RINS.
- To effectively modulate drifts of all three gyros.
- To address and mitigate horizontal velocity errors introduced by rotation strategies.
Main Methods:
- Implementation of a new dual-axis rotation strategy in a RINS.
- Experimental validation on a real dual-axis RINS.
- Detailed analysis of horizontal velocity errors and development of a calibration method.
Main Results:
- Reduced maximum azimuth angle error from 0.04° to less than 0.01° over 1 hour.
- Identified and analyzed sources of horizontal velocity errors.
- Achieved improved velocity precision by eliminating fluctuations and stages after calibration and compensation.
Conclusions:
- The proposed dual-axis rotation strategy effectively reduces azimuth angle errors in RINS.
- A new calibration method successfully mitigates velocity errors, enhancing overall INS performance.
- This work advances RINS accuracy for high-precision navigation applications.
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