TY - JOUR
T1 - Segmented Angular Rate Joint Estimation of Inertial Sensor Arrays for UAV Navigation
AU - Lu, Xin
AU - Zhang, Chunxi
AU - Li, Haoyang
AU - Yang, Yanqiang
AU - Li, Xianmu
AU - Cai, Xiaowen
N1 - Publisher Copyright:
© 1963-2012 IEEE.
PY - 2024
Y1 - 2024
N2 - A segmented angular rate joint estimator for fusing the measurements in an inertial sensor array is presented with higher precision and lower calculation burden, which offers better performance to unmanned aerial vehicle (UAV) navigation. In recent years, microaerial vehicles are increasingly indispensable in various industries. Attitude control is crucial for normal flight; therefore, the precision of angular rate measurement is the determinant for attitude calculation based on inertial measurement unit (IMU). The rapid development of MEMS industry, in addition to heterogeneous sensors, has given birth to multiple methods for improving the precision and reliability of angular rate measurement using homogeneous sensors called inertial sensor array. Computing angular motion based on inertial sensor array, including gyroscope and accelerometer triads, is a joint optimal estimation process. Due to the scale effect of accelerometer array, it is also sensitive to the angular motion. Both types of sensors can form a complementary filter at sensor level. In this article, we have proposed extended Kalman filter (EKF) and Levenberg-Marquardt (LM) framework for angular velocity estimate of inertial array system and fused them in the form of subsection measurement to give full play to the characteristics of the two methods and two types of sensors. Monte-Carlo simulation shows that the precision of angular velocity estimate is improved by up to 4.57%, and the calculation amount of the algorithm is greatly reduced.
AB - A segmented angular rate joint estimator for fusing the measurements in an inertial sensor array is presented with higher precision and lower calculation burden, which offers better performance to unmanned aerial vehicle (UAV) navigation. In recent years, microaerial vehicles are increasingly indispensable in various industries. Attitude control is crucial for normal flight; therefore, the precision of angular rate measurement is the determinant for attitude calculation based on inertial measurement unit (IMU). The rapid development of MEMS industry, in addition to heterogeneous sensors, has given birth to multiple methods for improving the precision and reliability of angular rate measurement using homogeneous sensors called inertial sensor array. Computing angular motion based on inertial sensor array, including gyroscope and accelerometer triads, is a joint optimal estimation process. Due to the scale effect of accelerometer array, it is also sensitive to the angular motion. Both types of sensors can form a complementary filter at sensor level. In this article, we have proposed extended Kalman filter (EKF) and Levenberg-Marquardt (LM) framework for angular velocity estimate of inertial array system and fused them in the form of subsection measurement to give full play to the characteristics of the two methods and two types of sensors. Monte-Carlo simulation shows that the precision of angular velocity estimate is improved by up to 4.57%, and the calculation amount of the algorithm is greatly reduced.
KW - Inertial sensor array
KW - segmented angular estimate (SAE)
KW - unmanned aerial vehicle (UAV) inertial measurement
UR - https://www.scopus.com/pages/publications/85187012240
U2 - 10.1109/TIM.2024.3370792
DO - 10.1109/TIM.2024.3370792
M3 - 文章
AN - SCOPUS:85187012240
SN - 0018-9456
VL - 73
SP - 1
EP - 14
JO - IEEE Transactions on Instrumentation and Measurement
JF - IEEE Transactions on Instrumentation and Measurement
M1 - 9506014
ER -