飞行器着舰碰撞动力学建模与仿真

Modeling and simulation of aircraft landing collision dynamics

本文对飞行器安全着舰问题进行研究。为有效分析飞行器与舰船发生碰撞时的相关参数,本文引入刚体碰撞运动理论,分别建立飞行器的运动模型和飞行器着舰动力学模型,并利用ADAMS软件对该模型进行仿真。仿真结果表明,该飞行器着舰动力模型能够对着舰时的相关参数进行有效计算与分析。

In this paper,the problem of aircraft safety landing ship was studied. In order to effectively analyze the related parameters of aircraft and ship collision,this paper introduced the theory of rigid body motion,the motion model of aircraft and aircraft landing dynamics models were established,and the model was simulated by using ADAMS software,the simulation results shown that the aircraft landing dynamic model to ship could effectively calculation and analysis related parameters.