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Acta Aeronautica et Astronautica Sinica ›› 2025, Vol. 46 ›› Issue (1): 630750.doi: 10.7527/S1000-6893.2024.30750

• Special Topic: Flexible Aerodynamic Deceleration Technologies • Previous Articles     Next Articles

Rigid-flexible coupling dynamic modeling for parachute cluster deceleration system

Haitao WANG1(), Jiangli LEI2, Wei RONG2   

  1. 1.College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China
    2.Beijing Institute of Space Mechanics and Electricity,Beijing 100094,China
  • Received:2024-05-30 Revised:2024-07-15 Accepted:2024-07-24 Online:2025-01-15 Published:2024-07-31
  • Contact: Haitao WANG E-mail:wanghaitao@nudt.edu.cn
  • Supported by:
    Laboratory Foundation of Aerospace Entry, Descent and Landing Technology(EDL-19092114);State Key Laboratory Foundation of Astronautic Dynamics(2022ADL-J006)

Abstract:

The parachute cluster deceleration system is widely used by the new generation reusable manned spacecraft, and dynamic analysis and evaluation of the parachute cluster system is an important task in the design and analysis of spacecraft deceleration missions. A multi-stage, variable structure and high-dimensional rigid-flexible coupling nonlinear multi-body dynamics model is established for the spacecraft parachute deceleration system. The characteristics of the system dynamics model are analyzed, and it is pointed out that the dynamics of the parachute cluster deceleration system have the dynamics properties of complex system. The dynamics and motion parameters of spacecraft, the drogue, and the main parachute are simulated and analyzed, and the results of Monte Carlo uncertainty simulation are summarized. The simulation and analysis results show that the established rigid-flexible coupling dynamic model can accurately simulate the working process of the parachute cluster deceleration system and the dynamic behavior of parachute group collisions. Finally, the existing problems and future developments in the dynamics of parachute deceleration systems are also discussed.

Key words: parachute cluster system, rigid-flexible coupling, complex system, dynamic modeling, deceleration

CLC Number: