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Published on: June 4, 2020
Precision and Error Propagation in Static MEMS-IMU Inertial Navigation: A Stochastic Time-Series Analysis
Mohammad Mahdi Kariminejad1, Mohammad Ali Sharifi1, Mir Abolfazl Mostafavi2
1School of Surveying and Geospatial Engineering, College of Engineering, University of Tehran, Tehran 1439957131, Iran.
This study analyzes errors in smartphone inertial navigation systems (MEMS-IMU) under static conditions. Results show raw sensor data is white noise, but derived position and velocity exhibit random walk errors.
Area of Science:
- Navigation Systems Engineering
- Sensor Data Analysis
- Robotics and Autonomous Systems
Background:
- Low-cost Microelectromechanical System Inertial Measurement Units (MEMS-IMUs) are increasingly used in navigation.
- Understanding their precision and error propagation under static conditions is crucial for reliable performance.
- Existing methods for error characterization require robust statistical frameworks.
Purpose of the Study:
- To investigate the precision and stochastic error propagation of navigation solutions from a MEMS-IMU using a smartphone.
- To develop and apply a comprehensive statistical framework for characterizing sensor and navigation state errors.
- To quantify the performance limitations of low-cost MEMS-IMUs in static scenarios.
Main Methods:
- Utilized a smartphone with MEMS-IMU rigidly mounted in a zero-reference scenario.
- Collected static inertial measurements, divided into statistically robust segments.
- Applied strapdown inertial mechanization to compute velocity and position.
- Employed statistical tests (ADF, Bartlett's, Ljung-Box) and ARIMA modeling for data analysis.
- Used power spectral density (PSD) and multivariate non-negative least squares variance component estimation (NNLS-VCE).
Main Results:
- Accelerometer and gyroscope data are characterized as stationary white-noise processes.
- Standard deviations for raw sensor data are ~10^-2 m/s^2 (accelerometer) and ~10^-4 rad/s (gyroscope).
- Derived velocity and position estimates exhibit random walk behavior, modeled by ARIMA(0,1,0) and ARIMA(0,2,0) respectively.
- After 30s, average standard deviations for ENU velocity and position estimates are σv=[0.77,0.44,0.29] m/s and σp=[1.30,0.69,0.46] m.
Conclusions:
- The proposed framework effectively models stochastic behavior and characterizes errors in low-cost MEMS-IMU navigation.
- Raw MEMS-IMU data behaves as white noise, but integration leads to significant random walk errors in velocity and position.
- This research provides a comprehensive approach for assessing the precision and performance of MEMS-IMU-based navigation systems.
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