Journal of Systems Engineering and Electronics ›› 2025, Vol. 36 ›› Issue (3): 814-824.doi: 10.23919/JSEE.2025.000066

• CONTROL THEORY AND APPLICATION • Previous Articles    

Field system-level calibration method for accelerometer considering nonlinear coefficients

Haotian WU(), Ruihang YU(), Juliang CAO(), Caixia MA(), Bainan YANG()   

  • Received:2024-01-22 Online:2025-06-18 Published:2025-07-10
  • Contact: Juliang CAO E-mail:674911458@qq.com;yuruihang@nudt.edu.cn;cjvl@163.com;18772667402@163.com;yang_cs_bn@163.com
  • About author:
    WU Haotian was born in 2001. He is a graduate student at National University of Defense Technology. His research interests are gravity measurement and integrated navigation. E-mail: 674911458@qq.com

    YU Ruihang was born in 1988. He received his Ph.D. degree from National University of Defense Technology. He is a professor in National University of Defense Technology. His research interests are gravity measurement and integrated navigation. E-mail: yuruihang@nudt.edu.cn

    CAO Juliang was born in 1976. He received his Ph.D. degree from National University of Defense Technology. He is a researcher in National University of Defense Technology. His research interests are gravity measurement and navigation technique. E-mail: cjvl@163.com

    MA Caixia was born in 1995. She received her M.D. degree from National University of Defense Technology. She is a researcher with Sirui Technology Co., Ltd. Her research interests are micro-electro-mechanical system calibration and navigation technique. E-mail: 18772667402@163.com

    YANG Bainan was born in 1995. He received his Ph.D. degree from National University of Defense Technology. He is an engineer in National University of Defense Technology University. His research interests are gravity measurement and navigation technique. E-mail: yang_cs_bn@163.com
  • Supported by:
    This work was supported by the National Natural Science Foundation of China (42276199).

Abstract:

In order to get rid of the dependence on high-precision centrifuges in accelerometer nonlinear coefficients calibration, this paper proposes a system-level calibration method for field condition. Firstly, a 42-dimension Kalman filter is constructed to reduce impact brought by turntable. Then, a biaxial rotation path is designed based on the accelerometer output model, including orthogonal 22 positions and tilt 12 positions, which enhances gravity excitation on nonlinear coefficients of accelerometer. Finally, sampling is carried out for calibration and further experiments. The results of static inertial navigation experiments lasting 4000 s show that compared with the traditional method, the proposed method reduces the position error by about 390 m.

Key words: accelerometer, nonlinear coefficient, system-level calibration, rotation path