Attitude Calculation of Quadrotor UAV Based on Extended Kalman Filter and Complementary Filter

نویسندگان

چکیده

Abstract Quadrotor UAV obtain the attitude calculation result from inertial measurement unit (IMU), but IMU has problems of high noise and low precision, to solve problems, this paper first introduces extended Kalman filter (EKF) complementary filter, uses them output accelerometer magnetic sensor. The effects two methods are compared by static testing dynamic testing. results show that both filtering can improve precision angle solutions, EKF algorithm performs better.

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ژورنال

عنوان ژورنال: Journal of physics

سال: 2023

ISSN: ['0022-3700', '1747-3721', '0368-3508', '1747-3713']

DOI: https://doi.org/10.1088/1742-6596/2460/1/012149