Volume 45 Issue 6
Jun.  2019
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YE Wen, CAI Chenguang, YANG Ping, et al. UKF estimation method incorporating Gaussian process regression[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1081-1087. doi: 10.13700/j.bh.1001-5965.2018.0591(in Chinese)
Citation: YE Wen, CAI Chenguang, YANG Ping, et al. UKF estimation method incorporating Gaussian process regression[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1081-1087. doi: 10.13700/j.bh.1001-5965.2018.0591(in Chinese)

UKF estimation method incorporating Gaussian process regression

doi: 10.13700/j.bh.1001-5965.2018.0591
Funds:

National Key R & D Program of China 2017YFF0205003

National Natural Science Foundation of China 61421063

National Natural Science Foundation of China 61722103

National Natural Science Foundation of China 61571030

National Natural Science Foundation of China 51605461

More Information
  • Corresponding author: YE Wen, E-mail: wenye@buaa.edu.cn
  • Received Date: 17 Oct 2018
  • Accepted Date: 11 Jan 2019
  • Publish Date: 20 Jun 2019
  • The high-precision filter estimation is a key technology in the SINS/GNSS integrated navigation system, and its estimation accuracy has direct influence on the accuracy of navigation. The traditional filter estimation method is based on inertial navigation error model, and does not take its uncertainty into account. Aimed at the problem, a high-precision filter estimation method is presented, which uses Gaussian process regression (GPR) to enhance the capabilities of prediction and estimation for parametric unscented Kalman filter (UKF). On one hand, it can estimate the state vector of the nonlinear parametric UKF on condition that trained data is limited; on the other hand, GPR can also take both the noise and the uncertainty in the nonlinear parametric UKF into consideration. The real vehicle-mounted experiment results show that the proposed method can effectively enhance filter estimation precision through applying the enhanced GPR-UKF into the SINS/GNSS integrated navigation system.

     

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