METHOD AND APPARATUS FOR YAW FUSION AND AIRCRAFT

    公开(公告)号:US20220155800A1

    公开(公告)日:2022-05-19

    申请号:US17649831

    申请日:2022-02-03

    Abstract: Embodiments of the present invention relates to a method and apparatus for yaw fusion and an aircraft. The method includes: acquiring magnetometer data, inertial measurement unit (IMU) data, and global positioning system (GPS) data; determining a yaw angular velocity correction amount according to the GPS data and the magnetometer data; determining a first yaw angular velocity error value according to the IMU acceleration information and the GPS acceleration information; determining an initial complementary fusion yaw angular velocity; determining a second yaw angular velocity error value; and determining a final complementary fusion yaw.

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