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Keeping a Good Attitude: A Quaternion-Based Orientation Filter for IMUs and MARGs
Roberto G Valenti1, Ivan Dryanovski2, Jizhong Xiao3
1The City College of New York, The City University of New York, Convent Avenue and 140th Street, New York, NY 10031, USA. robertogl.valenti@gmail.com.
This study presents a new method for estimating Micro Aerial Vehicle (MAV) orientation using low-cost sensors. The novel approach improves accuracy by separating tilt and heading estimations, outperforming existing methods.
Area of Science:
- Robotics and Control Systems
- Sensor Fusion and Estimation Theory
- Aerospace Engineering
Background:
- Accurate orientation estimation is critical for Micro Aerial Vehicles (MAVs) attitude control.
- Low-cost MicroElectroMechanical System (MEMS) inertial sensors present challenges due to low accuracy and noisy data.
- Existing methods struggle with magnetic disturbances affecting orientation estimation.
Purpose of the Study:
- To develop a novel quaternion-based orientation estimation method for MAVs.
- To address the impact of magnetic disturbances on roll and pitch orientation.
- To propose a new complementary filter fusing gyroscope, accelerometer, and magnetometer data.
Main Methods:
- Algebraic solution for orientation estimation using gravity and magnetic field observations.
- Separation of 'tilt' and 'heading' quaternion estimation to mitigate magnetic interference.
- Development of a novel complementary filter integrating gyroscope, accelerometer, and magnetometer data for IMU and MARG sensors.
Main Results:
- Analytical and empirical validation of the proposed orientation estimation method.
- Demonstrated significant performance improvement over common orientation estimation techniques.
- Successful evaluation using real-world flight data from a micro quadrotor helicopter.
Conclusions:
- The proposed method effectively estimates MAV orientation, even with low-cost sensors.
- The novel complementary filter provides superior performance compared to existing methods.
- This approach enhances MAV attitude control by providing reliable orientation feedback.
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