Abstract
The parachute system in the steady descent phase consists of four main parachutes, riser, artillery cargo and so on, is a typical multibody system. In this paper, a parachute cluster dynamics model considering the contact collision between each main parachute is first established based on the reduced multibody transfer matrix method (RMSTMM) which is no need for global dynamic equations and has high computational speed. The dynamics responses of the cargo are compared with Newton–Euler method under the wind condition. The dynamics model for parachute cluster established by RMSTMM is validated. The research of this paper lays a foundation for rapid modelling and simulation of the cargo airdrop.
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References
Ibrahim SK, Engdahl RA (1974) Parachute dynamics and stability analysis
Talay TA (1974) Parachute-deployment-parameter identification based on an analytical simulation of Viking BLDT AV-4
Wolf DF, Spahr HR (1977) Parachute cluster dynamic analysis. J Aircr 14(4):321–322
He M, Tang S, Xu Z (2010) Modeling and analysis of rocket-parachute system dynamics based on Kane method. Flight Dyn 28(05):39–42
Cheng YK, Yang XW, Chen XL (1998) The equations of motion for a parachute. Spacecraft Recovery Remote Sens 19(1):1–4
Zhu Y, Liu L (2009) Dynamic model of parachute-projectile systems based on lagrange mechanics. Acta Aeronautica et Astronautica Sinica 30(7):1208–1231
Ning LM (2018) High-fidelity flight simulation of parachute-payload system: the multibody dynamics approach and fluid-structure interaction approach. Nan**g University of Aeronautics and Astronautics
Rui XT, Zhang JS, Wang X et al (2022) Multibody system transfer matrix method: the past, the present, and the future. Int J Mech Syst Dyn 2(1):3–26
Wang GP, Tao L, Rong B et al (2023) Review of dynamics simulation methods for multi-field coupling systems. Adv Mech 53(2):4
Lu HJ, Rui XT, Ma ZY et al (2022) Hybrid multibody system method for the dynamic analysis of an ultra-precision fly-cutting machine tool. Int J Mech Syst Dyn 2(3):290–307
Bestle D (2021) Eigenvalue sensitivity analysis based on the transfer matrix method. Int J Mech Syst Dyn 1(1):96–107
Rui X, Bestle D, Wang G et al (2021) Reduced multibody system transfer matrix method using decoupled hinge equation. Int J Mech Syst Dyn 1(2):182–193
Acknowledgements
This work was supported by National Natural Science Foundation of China (No. 11972193 and No. 92266201), China Postdoctoral Science Foundation (2022M720066), Jiangsu Funding Program for Excellent Postdoctoral Talent.
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Wang, Y., Wang, G., Sun, Y., Han, C., Gu, L. (2024). Dynamics Modelling and Simulation of Parachute Cluster Based on Rmstmm. In: Rui, X., Liu, C. (eds) Proceedings of the 2nd International Conference on Mechanical System Dynamics. ICMSD 2023. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-99-8048-2_154
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DOI: https://doi.org/10.1007/978-981-99-8048-2_154
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