基于飞机动力学建模的无动力空投浮标仿真与预测方法

Xin Wu, Zhaohong Wang, Zhangpeng Tu, Yuanchao Zhu, Weitao Wu, Yulu Chen, Puzhe Zhou, Canjun Yang
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引用次数: 0

摘要

无动力空投是海洋研究中广泛使用的一种部署浮标的方式。本文提出了一种通过数值模拟来预测无动力空投浮标运动轨迹和速度的方法。参考飞机动力学建立了空投浮标的微分动力学模型,该模型包含了浮标的动力学、运动学和几何约束。利用XFlow软件计算并得到了相应的浮筒气动超参数。尽管不同几何形状和质量分布的浮标需要重新计算特定的气动系数值,但所提出的建模范式总是适用的。仿真结果显示了浮标的运动轨迹和速度特性,为空投释放和降落伞打开时机的把握提供了指导。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Simulation and Prediction Method for Unpowered Airdropped Buoys Based on Aircraft Dynamics Modeling
Unpowered airdrop is a widely used way to deploy buoys in marine research. This paper presents a method to predict the trajectory and the velocity of unpowered airdropped buoys through numerical simulation. A differential dynamic model of the airdropped buoy is established with reference to the aircraft dynamics, which contains the kinetics, kinematics, and geometric constraints of the buoy. The corresponding aerodynamic hyperparameters of the buoy are calculated and obtained by XFlow software. Although specific aerodynamic coefficient values need to be recalculated for buoys with different geometries and mass distributions, the proposed modeling paradigm is always applicable. The simulation results show the trajectory and velocity characteristics of the buoy, which provide guidance for grasping the timing of airdrop release and parachute opening.
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