TY - GEN
T1 - State Estimator of Errorekf and UKF Based on Generalized-A Method for Constrained Multibody Systems
AU - Hao, Yutao
AU - Zhou, Liliang
AU - Zhang, Huan
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - Multibody dynamics models inherently contain comprehensive physical information of complex systems, while multibody integrators enable efficient prediction of dynamic behaviors. The advancements in these two research interests have made it a natural progression to integrate multibody dynamics models and multibody integrators into state estimators. However, their integration faced several challenges: nonlinear discrete formulations, reformulation of differential-algebraic equations (DAEs), constraint violation correction, and integrator selection. With ongoing research, the first three issues have been largely resolved for low-order rigid multibody systems. Nevertheless, current one-step prediction methods predominantly rely on explicit integrators or low-order implicit integrators, which suffer from inefficiencies in state estimation and inadequate constraint violation correction. This study proposes the framework that embeds the generalized-α integrator - a high-order multibody integrator - within the error Extended Kalman filter(errorEKF) architecture and Unscented Kalman filter(UKF). The generalized-α integrator is employed for one-step state prediction which directly solves the original DAEs, ensuring that states remain strictly on the constraint manifold. Comparative studies with this two Kalman filter-based state estimators are conducted on two benchmarks: a four-bar mechanism and a five-bar mechanism. The results shown that both state estimators based on the generalized-α integration method have good estimation accuracy. In terms of computational efficiency, the estimated computational efficiency of ErrEKF is significantly higher than that of UKF.
AB - Multibody dynamics models inherently contain comprehensive physical information of complex systems, while multibody integrators enable efficient prediction of dynamic behaviors. The advancements in these two research interests have made it a natural progression to integrate multibody dynamics models and multibody integrators into state estimators. However, their integration faced several challenges: nonlinear discrete formulations, reformulation of differential-algebraic equations (DAEs), constraint violation correction, and integrator selection. With ongoing research, the first three issues have been largely resolved for low-order rigid multibody systems. Nevertheless, current one-step prediction methods predominantly rely on explicit integrators or low-order implicit integrators, which suffer from inefficiencies in state estimation and inadequate constraint violation correction. This study proposes the framework that embeds the generalized-α integrator - a high-order multibody integrator - within the error Extended Kalman filter(errorEKF) architecture and Unscented Kalman filter(UKF). The generalized-α integrator is employed for one-step state prediction which directly solves the original DAEs, ensuring that states remain strictly on the constraint manifold. Comparative studies with this two Kalman filter-based state estimators are conducted on two benchmarks: a four-bar mechanism and a five-bar mechanism. The results shown that both state estimators based on the generalized-α integration method have good estimation accuracy. In terms of computational efficiency, the estimated computational efficiency of ErrEKF is significantly higher than that of UKF.
KW - error Extended Kalman filter(errorEKF)
KW - generalized-α integration method
KW - multibody model
KW - state estimator
KW - Unscented Kalman filter(UKF)
UR - https://www.scopus.com/pages/publications/105030437573
U2 - 10.1109/CoMEA66280.2025.11241648
DO - 10.1109/CoMEA66280.2025.11241648
M3 - Conference contribution
AN - SCOPUS:105030437573
T3 - Proceedings of 2025 International Conference of Mechanical Engineering on Aerospace, CoMEA 2025
BT - Proceedings of 2025 International Conference of Mechanical Engineering on Aerospace, CoMEA 2025
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2025 International Conference of Mechanical Engineering on Aerospace, CoMEA 2025
Y2 - 20 June 2025 through 22 June 2025
ER -