TY - GEN
T1 - Augmented Robust Cubature Kalman Filter Applied in Re-Entry Vehicle Tracking
AU - Li, Shoupeng
AU - Wang, Pu
AU - Mu, Rongjun
AU - Cui, Naigang
N1 - Publisher Copyright:
© 2021 IEEE.
PY - 2021/3/6
Y1 - 2021/3/6
N2 - In this work, an improved cubature Kalman filter (CKF), called augmented robust CKF (ARCKF), for the reentry vehicle trajectory tracking is presented, in which the model strong nonlinearity, heavy-tailed measurement noise, and the non-independence of measurement noise in iterations are considered. Firstly, the derivative-free robust approach is employed instead of the conventional Huber's technique, thereby eliminating linearization errors and exhibiting robustness to measurement outliers. Secondly, the framework of iterated unscented Kalman filter is adopted to avoid linearization in the iterative measurement update, in which new cubature sample points are regenerated in each iteration, and then the probability density function is propagated through the measurement model. Furthermore, in the measurement update stage, the state vector is augmented with the measurement noise vector to address their correlation after the first iteration. To demonstrate the validity of the proposed algorithm, CKF, robust CKF (RCKF), and ARCKF are compared via Monte Carlo simulations. The results show that ARCKF performs with sufficient suitability in non-Gaussian noise environments and is superior in terms of target tracking accuracy.
AB - In this work, an improved cubature Kalman filter (CKF), called augmented robust CKF (ARCKF), for the reentry vehicle trajectory tracking is presented, in which the model strong nonlinearity, heavy-tailed measurement noise, and the non-independence of measurement noise in iterations are considered. Firstly, the derivative-free robust approach is employed instead of the conventional Huber's technique, thereby eliminating linearization errors and exhibiting robustness to measurement outliers. Secondly, the framework of iterated unscented Kalman filter is adopted to avoid linearization in the iterative measurement update, in which new cubature sample points are regenerated in each iteration, and then the probability density function is propagated through the measurement model. Furthermore, in the measurement update stage, the state vector is augmented with the measurement noise vector to address their correlation after the first iteration. To demonstrate the validity of the proposed algorithm, CKF, robust CKF (RCKF), and ARCKF are compared via Monte Carlo simulations. The results show that ARCKF performs with sufficient suitability in non-Gaussian noise environments and is superior in terms of target tracking accuracy.
UR - https://www.scopus.com/pages/publications/85111354294
U2 - 10.1109/AERO50100.2021.9438506
DO - 10.1109/AERO50100.2021.9438506
M3 - 会议稿件
AN - SCOPUS:85111354294
T3 - IEEE Aerospace Conference Proceedings
BT - 2021 IEEE Aerospace Conference, AERO 2021
PB - IEEE Computer Society
T2 - 2021 IEEE Aerospace Conference, AERO 2021
Y2 - 6 March 2021 through 13 March 2021
ER -