TY - GEN
T1 - On-line orientation calibration of Inertial Measurement Unit pairs using unmanned aerial vehicle flight data
AU - Lassak, Kyle
AU - Rhudy, Matthew
AU - Gu, Yu
PY - 2013/9/16
Y1 - 2013/9/16
N2 - Calibration of the orientation of multiple Inertial Measurement Unit (IMU) pairs was performed using flight data collected from six separate flights by the West Virginia University (WVU) 'Red Phastball' Unmanned Aerial Vehicle (UAV). Four closely grouped IMUs were located in the front of the UAV for all six flights, and two sets of flight data featured a fifth IMU positioned at the rear of the UAV. This enabled calibration of IMU pairs with negligible distance as well as calibration of spatially separated IMUs, which were modeled assuming rigid body mechanics. Accelerometer and rate gyroscope data were used to produce two linearly independent vectors which were used to define the relative orientation of each IMU pair via an Unscented Kalman Filter (UKF). Using static UAV data recorded before each flight, the gravity vector was used for off-line calibration of the pitch and roll of each IMU with respect to the Earth reference frame, which was used as a truth reference to evaluate the accuracy of the on-line calibration techniques.
AB - Calibration of the orientation of multiple Inertial Measurement Unit (IMU) pairs was performed using flight data collected from six separate flights by the West Virginia University (WVU) 'Red Phastball' Unmanned Aerial Vehicle (UAV). Four closely grouped IMUs were located in the front of the UAV for all six flights, and two sets of flight data featured a fifth IMU positioned at the rear of the UAV. This enabled calibration of IMU pairs with negligible distance as well as calibration of spatially separated IMUs, which were modeled assuming rigid body mechanics. Accelerometer and rate gyroscope data were used to produce two linearly independent vectors which were used to define the relative orientation of each IMU pair via an Unscented Kalman Filter (UKF). Using static UAV data recorded before each flight, the gravity vector was used for off-line calibration of the pitch and roll of each IMU with respect to the Earth reference frame, which was used as a truth reference to evaluate the accuracy of the on-line calibration techniques.
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M3 - Conference contribution
SN - 9781624102240
T3 - AIAA Guidance, Navigation, and Control (GNC) Conference
BT - AIAA Guidance, Navigation, and Control (GNC) Conference
T2 - AIAA Guidance, Navigation, and Control (GNC) Conference
Y2 - 19 August 2013 through 22 August 2013
ER -