The results of this model provide an important foundation for fuselage and arresting hook device design.
该模型的结果为机身和拦阻钩装置的设计提供了重要依据。
Then the motion equations of an arresting hook engaging an arresting cable directly and indirectly are presented.
建立了拦阻索直接上钩和间接上钩时拦阻钩的运动方程，分析了此时拦阻索上钩时拦阻钩运动特性。
The conventional and carrier variants provide a button to drop and raise the arresting hook for carrier and emergency landings.
常规及舰载型号将提供一个按钮来收放着舰时和紧急着陆情况下的阻拦索捕捉钩。
Then the kinematics equations of arresting hook in regular runway and irregular runway are established and the bounce characteristic is analyzed.
建立了飞机拦阻钩在光滑道面上以及不规则道面上的弹跳运动方程，分析了拦阻钩的弹跳特性以及运动特性。
In this article, a study is made of the collision dynamics of the arresting hook bounce after initial touchdown when the aircraft is arrested, and a collision bounce model is built.
分析了飞机着舰拦阻时，拦阻钩初次接触道面碰撞后被反弹的动力学成因，建立了飞机拦阻钩碰撞道面的弹跳模型。
In this article, a study is made of the collision dynamics of the arresting hook bounce after initial touchdown when the aircraft is arrested, and a collision bounce model is built.
分析了飞机着舰拦阻时，拦阻钩初次接触道面碰撞后被反弹的动力学成因，建立了飞机拦阻钩碰撞道面的弹跳模型。
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