An In-Bore Projectile and a Flexible Tube Seen as a Superelement in Launch Dynamics Using Reduced Multibody System Transfer Matrix Method
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-8048-2_148
Reference11 articles.
1. Rui X (2015) Launch dynamics of multibody systems (in Chinese). National Defense Industry Press, Beijing
2. Rui X, Zhang J, Wang X, Rong B, He B, Jin Z (2022) Multibody system transfer matrix method: The past, the present, and the future. Int J Mechan Syst Dyn 2(1):3–26. https://doi.org/10.1002/msd2.12037
3. Zhou Q, Rui X, Wang G, Zhang J (2021) An efficient and modular modeling for launch dynamics of tubed rockets on a moving launcher. Defence Technol 17(6):2011–2026. https://doi.org/10.1016/j.dt.2020.10.005
4. Yu H, Rui X (2014) Study on launch dynamics of self-propelled artillery based on transfer matrix method of multibody System. Adv Mech Eng 6:308049. https://doi.org/10.1155/2014/308049
5. Rui X, Bestle D (2021) Reduced multibody system transfer matrix method using decoupled hinge equations. Int J Mechan Syst Dyn 1(2):182–193. https://doi.org/10.1002/msd2.12026
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