Modeling and analysis of landing collision dynamics for a shipborne helicopter

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机械工程前沿（英文）

2021年第16卷第1期页码 151-162

Modeling and analysis of landing collision dynamics for a shipborne helicopter

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10.1007/s11465-020-0617-z

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摘要

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.

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shipborne helicopter ; landing model ; Lagrange equations ; dynamics ; validation

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机械工程前沿（英文）

Modeling and analysis of landing collision dynamics for a shipborne helicopter

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大纲

Figures(5)

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其他(2)

机械工程前沿（英文）

Modeling and analysis of landing collision dynamics for a shipborne helicopter

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评论

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