Frontiers of Mechanical Engineering >
Modeling and analysis of landing collision dynamics for a shipborne helicopter
Received date: 30 Jul 2020
Accepted date: 25 Oct 2020
Published date: 15 Mar 2021
Copyright
A Lagrange dynamic model is established based on small-angle approximation to improve the simulation model for shipborne helicopter landing collision. To describe fuselage motion effectively, the proposed model considers ship motion, the interaction of the tires with the deck, and tire slippage. A mechanism of sliding motion is built, and a real-time reliability analysis of the algorithm is implemented to validate the proposed model. Numerical simulations are also conducted under different operation conditions. Results show that the proposed dynamic model can simulate the collision motion of helicopter landing in real time. Several suggestions for helicopter pilot landing are likewise provided.
Key words: shipborne helicopter; landing model; Lagrange equations; dynamics; validation
Dingxuan ZHAO , Haojie YANG , Carbone GIUSEPPE , Wenhang LI , Tao NI , Shuangji YAO . Modeling and analysis of landing collision dynamics for a shipborne helicopter[J]. Frontiers of Mechanical Engineering, 2021 , 16(1) : 151 -162 . DOI: 10.1007/s11465-020-0617-z
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