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Optimal trajectory planning for flexible truss assembly based on nonlinear model predictive control

  • Qingsheng Wei
  • , Ye Gao
  • , Jiabo Jiang
  • , Yatao Zhao*
  • , Cheng Wei
  • *Corresponding author for this work
  • School of Astronautics, Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

With the continuous advancement of space technology, on-orbit assembly of truss structures using robotic manipulators is expected to become an important development trend. Unlike rigid payloads, large-scale lightweight trusses exhibit significant elastic vibrations during assembly, which can compromise end-effector accuracy and increase the risk of structural fatigue if they are not adequately suppressed. This paper proposes an optimal vibration-suppression trajectory-planning method for robotic manipulators assembling flexible truss structures. First, a rigid–flexible coupled dynamic model of the robot–truss system is established, and the interaction between manipulator end-effector motion and truss vibration is derived in task space. On this basis, a nonlinear model predictive control (NMPC) framework is formulated to optimize the assembly trajectory subject to vibration-suppression objectives, actuator limits, workspace constraints, and obstacle-avoidance requirements. By jointly penalizing terminal-state errors, structural modal responses, and control-input variations, the proposed method reduces modal excitation during trajectory generation. In the numerical study, the NMPC problem is solved sequentially in a receding-horizon manner using the current simulated state; however, no hard real-time computation deadline is imposed. In the physical experiments, the trajectories are generated offline and subsequently executed by the manipulator’s low-level position controller. The simulation and experimental results show that the proposed approach reduces multi-modal vibration, generates smooth and collision-free end-effector motion, and outperforms the considered non-optimized trajectory-planning baselines.

Original languageEnglish
Article number113324
JournalAerospace Science and Technology
Volume179
DOIs
StatePublished - Dec 2026
Externally publishedYes

Keywords

  • Nonlinear model predictive control,
  • On-orbit assembly
  • Trajectory planning
  • Vibration suppression

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