Application of an off-the-shelf Fiber Optic Gyroscope based Inertial Measurement Unit for attitude and heading estimation
Alexander Albrecht, Janko Petereit
Abstract
Alexander Albrecht, Janko Petereit
Abstract
The ability to estimate attitude (pitch, roll) and heading (yaw) in reference to the North-East-Down frame is of great importance for localization applications. Determining true north proves to be especially challenging. This paper presents a fast and simple north-seeking method by utilizing earth's rotation measured by a three-axis Inertial Measurement Unit (IMU) based on Fiber Optic Gyroscopes (FOG) and Micro-Electro-Mechanical Systems (MEMS) accelerometers. Assuming a non-moving IMU, its measured accelerations and angular velocities are solely evoked by earth's gravitation and angular speed. To increase accuracy, a static multi-position calibration scheme is introduced. Sensor bias is estimated under the assumption that the magnitude of accelerometer and gyroscope data equals earth's gravitation and angular speed. Precision and accuracy of the gyrocompass is experimentally evaluated and prove to be a promising alternative in comparison to expensive commercially available Attitude and Heading Reference Systems (AHRS).
OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
The ability to estimate attitude (pitch, roll) and heading (yaw) in reference to the North-East-Down frame is of great importance for localization applications. Determining true north proves to be especially challenging. This paper presents a fast and simple north-seeking method by utilizing earth's rotation measured by a three-axis Inertial Measurement Unit (IMU) based on Fiber Optic Gyroscopes (FOG) and Micro-Electro-Mechanical Systems (MEMS) accelerometers. Assuming a non-moving IMU, its measured accelerations and angular velocities are solely evoked by earth's gravitation and angular speed. To increase accuracy, a static multi-position calibration scheme is introduced. Sensor bias is estimated under the assumption that the magnitude of accelerometer and gyroscope data equals earth's gravitation and angular speed. Precision and accuracy of the gyrocompass is experimentally evaluated and prove to be a promising alternative in comparison to expensive commercially available Attitude and Heading Reference Systems (AHRS).
Key concepts: Gyroscope, Attitude and heading reference system, Accelerometer, Inertial measurement unit, Heading (navigation), Angular velocity, Rotation (mathematics), Inertial navigation system