• Electronics Optics & Control
  • Vol. 28, Issue 2, 75 (2021)
YANG Songpu1, YAN Fei2, and ZHU Hai3
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2021.02.015 Cite this Article
    YANG Songpu, YAN Fei, ZHU Hai. An Attitude Estimation Algorithm of AHRS Under Influence of Maneuvering Acceleration[J]. Electronics Optics & Control, 2021, 28(2): 75 Copy Citation Text show less
    References

    [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.

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    [1] LIU Kangan, ZHANG Weiwei, XIAO Yongchao, YE Mu. Attitude Calculation of Quadrotor UAV Based on Adaptive Unscented Kalman Filter[J]. Electronics Optics & Control, 2022, 29(7): 126

    YANG Songpu, YAN Fei, ZHU Hai. An Attitude Estimation Algorithm of AHRS Under Influence of Maneuvering Acceleration[J]. Electronics Optics & Control, 2021, 28(2): 75
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