TY - GEN
T1 - A Comparison of Numerical Integration Algorithms for Flexible Variable-Length Cable Multibody Dynamics
AU - Su, Jingkai
AU - Qi, Liuzhelie
AU - Zhang, Huan
N1 - Publisher Copyright:
© 2025 IEEE.
PY - 2025
Y1 - 2025
N2 - Flexible cables exhibit advantages such as high flexibility, superior strength, and ease of altering force transmission directions, making them widely applicable in aerospace and civil fields, including large deployable antennas, cable-driven parallel robots for in-orbit operations, and cranes. Motor-driven winches are commonly combined with flexible cables, resulting in variable-length characteristics. For cable systems featuring large deformations and time- varying lengths, the arbitrary Lagrangian-Eulerian (ALE) description method under the Absolute Nodal Coordinate Formulation (ANCF) framework is particularly suitable for modeling them as differential-algebraic equations (DAEs) with constraints. This study aims to compare the capabilities of several numerical methods in representing the dynamic characteristics of such systems, including accuracy, stability, computational efficiency, and constraint violation correction. The evaluated methods include the Runge-Kutta method, generalized-alpha method, and backward differentiation formula (BDF) method. Numerical simulations under multiple working conditions yield the following conclusions: All three methods stably generate accurate dynamic results for flexible variable-length cables. Regarding constraint violation correction, the generalized-alpha and BDF methods demonstrate higher accuracy without requiring the conversion of DAEs into ordinary differential equations. In terms of step size, the generalized-alpha method allows larger time steps. However, the Runge-Kutta method exhibits superior computational efficiency. The generalized-alpha method strikes a balance for scenarios requiring strict constraint enforcement and moderate computational resources, whereas the Runge-Kutta method is preferable for efficiency-critical applications with minor constraint violations.
AB - Flexible cables exhibit advantages such as high flexibility, superior strength, and ease of altering force transmission directions, making them widely applicable in aerospace and civil fields, including large deployable antennas, cable-driven parallel robots for in-orbit operations, and cranes. Motor-driven winches are commonly combined with flexible cables, resulting in variable-length characteristics. For cable systems featuring large deformations and time- varying lengths, the arbitrary Lagrangian-Eulerian (ALE) description method under the Absolute Nodal Coordinate Formulation (ANCF) framework is particularly suitable for modeling them as differential-algebraic equations (DAEs) with constraints. This study aims to compare the capabilities of several numerical methods in representing the dynamic characteristics of such systems, including accuracy, stability, computational efficiency, and constraint violation correction. The evaluated methods include the Runge-Kutta method, generalized-alpha method, and backward differentiation formula (BDF) method. Numerical simulations under multiple working conditions yield the following conclusions: All three methods stably generate accurate dynamic results for flexible variable-length cables. Regarding constraint violation correction, the generalized-alpha and BDF methods demonstrate higher accuracy without requiring the conversion of DAEs into ordinary differential equations. In terms of step size, the generalized-alpha method allows larger time steps. However, the Runge-Kutta method exhibits superior computational efficiency. The generalized-alpha method strikes a balance for scenarios requiring strict constraint enforcement and moderate computational resources, whereas the Runge-Kutta method is preferable for efficiency-critical applications with minor constraint violations.
KW - constraint violation correction
KW - flexible variable-length cable
KW - multibody dynamics
KW - numerical integration
UR - https://www.scopus.com/pages/publications/105030468866
U2 - 10.1109/CoMEA66280.2025.11241246
DO - 10.1109/CoMEA66280.2025.11241246
M3 - Conference contribution
AN - SCOPUS:105030468866
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 -