[3] POURTAKDOUST S H,ASL H G.An adaptive unscented Kalman filter for quaternion-based orientation estimation in low-cost AHRS[J].Aircraft Engineering and Aerospace Technology,2007,79(5): 485-493.
[4] AHMED H,TAHIR M.Accurate attitude estimation of a moving land vehicle using low-cost MEMS IMU sensors[J].IEEE Transactions on Intelligent Transportation System, 2017,18(7): 1723-1739.
[5] XING L,HANG Y J,XIONG Z.Accurate attitude estimation using ARS under conditions of vehicle movement based on disturbance acceleration adaptive estimation and correction[J].Sensors,2016,16(3): 1716-1732.
[6] WANG M L,WANG H.An adaptive attitude algorithm based on a current statistical model for maneuvering acceleration[J].Chinese Journal of Aeronautics,2017,30(1): 426-433.
[7] LEE J K,PARK E,ROBINOVITCH S.Estimation of attitude and external acceleration using inertial sensor mea-surement during dynamic conditions[J].IEEE Transactions on Instrumentation and Measurement,2012,61(8): 2262-2273.
[8] SABATINI A M.Quaternion-based extended Kalman filter for determining orientation by inertial and magnetic sensing[J].IEEE Transactions on Biomedical Engineering, 2006,53(7): 1346-1356.