Attitude and heading measurement based on adaptive complementary Kalman filter for PS/MIMU integrated system
This study introduces an adaptive complementary Kalman filter (ACKF) for unmanned vehicles, enhancing attitude and heading accuracy using bionic polarization sensors and MEMS inertial measurement units, even without GPS. The ACKF method significantly improves system performance in challenging environments.
Area of Science:
- Robotics and Autonomous Systems
- Sensor Fusion and Navigation
Background:
- Unmanned vehicles require reliable attitude and heading information, especially when Global Navigation Satellite System (GNSS) is unavailable.
- Existing bionic polarization sensor (PS)/MEMS inertial measurement unit (MIMU) systems struggle in harsh environments (inclining, sheltering) due to underutilization of sensor complementarity.
- Current methods limit system performance by not fully leveraging the synergistic characteristics of gyroscopes, accelerometers, and PS.
Purpose of the Study:
- To propose an improved attitude and heading measurement method for unmanned vehicles.
- To enhance system adaptability and accuracy in challenging environmental conditions.
- To fully exploit the complementary nature of gyroscopes, accelerometers, and polarization sensors.
Main Methods:
- Development of an adaptive complementary Kalman filter (ACKF) for attitude and heading estimation.
- Correction of gyroscope data using accelerometer-measured gravity for improved attitude accuracy.
- Fusion of IMU heading and tilt-compensated polarization heading via Kalman optimal estimation.
- Construction of an adaptive factor using maximum correlation entropy between measured and theoretical gravity for adaptive sensor complementarity.
Main Results:
- The proposed ACKF method demonstrated effectiveness in both outdoor rotation and vehicle occlusion tests.
- Significant reductions in Root Mean Square Error (RMSE) were observed for pitch (89.3%), roll (93.2%), and heading (9.6%) compared to traditional Kalman filters during vehicle testing.
- The method shows great advantages in improving the accuracy and reliability of attitude and heading information.
Conclusions:
- The adaptive complementary Kalman filter (ACKF) effectively addresses the limitations of existing methods for attitude and heading determination in GNSS-denied environments.
- The ACKF enhances system performance by adaptively fusing data from PS, gyroscopes, and accelerometers, improving robustness in harsh conditions.
- This approach offers a significant advancement for navigation systems in unmanned vehicles, particularly under challenging operational scenarios.
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