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Dynamic analysis of rigid-flexible coupling spacecraft based on Euler parameters.

Yi Ji1,2,3, Huan Zhang4

  • 1School of Astronautics, Harbin Institute of Technology, Harbin, 150001, China.

Scientific Reports
|May 3, 2025
PubMed
Summary
This summary is machine-generated.

This study introduces a new numerical method for analyzing spacecraft dynamics. The BN-stable method, enhanced for rigid-flexible coupling, offers superior accuracy and stability for complex aerospace simulations.

Keywords:
BN-stabilityDynamic analysisEuler parametersRigid-flexible couplingRotation matrix

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Area of Science:

  • Aerospace Engineering
  • Computational Mechanics
  • Nonlinear Dynamics

Background:

  • Modern spacecraft feature complex rigid-flexible coupling, posing significant challenges for dynamic analysis.
  • Existing numerical tools struggle with the strong nonlinearity inherent in these systems.

Purpose of the Study:

  • To develop an accurate and efficient numerical method for analyzing the dynamic behavior of rigid-flexible coupling spacecraft.
  • To address the limitations of current tools in handling highly nonlinear dynamic systems.

Main Methods:

  • Described rigid and flexible bodies using Euler parameters to avoid singular angles.
  • Applied a reformulated BN-stable method, ensuring unconditional stability for nonlinear initial value problems.
  • Incorporated angular velocity-Euler parameter relations and velocity-level constraints to maintain numerical rotation matrix accuracy.

Main Results:

  • The proposed strategy effectively simulates the dynamic responses of spacecraft, including rigid bodies and flexible solar wings.
  • Demonstrated considerable advantages in accuracy, stability, and dissipation compared to existing popular strategies.
  • Validated the enhanced BN-stable method for transient response analysis of nonlinear systems.

Conclusions:

  • The reformulated BN-stable method provides a robust and accurate solution for analyzing rigid-flexible coupling spacecraft dynamics.
  • This approach overcomes key challenges associated with strong nonlinearity in aerospace simulations.
  • Offers a significant improvement over conventional methods for spacecraft dynamic analysis.