Abstract
Extreme orbital thermal cycling and temperature-dependent clearance nonlinearity make it difficult to predict contact–impact, stick–slip, and bifurcation responses of flexible deployable space structures with sufficient stability, accuracy, and computational efficiency. An Adaptive Dissipation–Precision Coordinated Multi-Scale Implicit Integration Algorithm (ADPC-MSIIA) is proposed. First, an absolute nodal coordinate formulation (ANCF)-based thermo-mechanical clearance-joint model with thermal-viscosity-modified contact and frictional/impact heat feedback is established; second, a dual-time-scale implicit integration scheme with dual- (Formula presented.) stability–dissipation control and third-order compensation is developed; finally, numerical validation is performed using a linear single-degree-of-freedom (SDOF) benchmark, a temperature-dependent clearance impact oscillator, finite-element and published benchmark comparisons, and a deployable annular truss antenna case. Simulation results show that ADPC-MSIIA achieves a high-frequency spectral radius of (Formula presented.), an effective convergence order of (Formula presented.), a maximum contact force error of (Formula presented.), and a (Formula presented.) reduction in the global cumulative error compared with the generalized- (Formula presented.) method. This study contributes to knowledge by linking temperature-driven clearance evolution, frictional heat feedback, and adaptive numerical dissipation within a unified framework for predicting non-smooth thermo-mechanical deployment dynamics of large flexible space structures with clearance joints.
| Original language | English |
|---|---|
| Article number | 5461 |
| Journal | Applied Sciences (Switzerland) |
| Volume | 16 |
| Issue number | 11 |
| DOIs | |
| State | Published - Jun 2026 |
| Externally published | Yes |
Keywords
- adaptive time integration
- clearance joint
- deployable space structure
- flexible multibody dynamics
- numerical dissipation control
- thermo-mechanical coupling
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