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空降车辆着陆缓冲过程系统建模仿真研究综述
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作者 石坚 杨占华 +3 位作者 刘春生 郭少鹏 柴辉 于贵申 《兵器装备工程学报》 CAS CSCD 北大核心 2024年第9期104-115,共12页
系统建模仿真作为空降车辆着陆缓冲研究的重要手段,用于仿真着陆缓冲阶段的气囊排气压缩、车辆缓冲过载、姿态变化及结构冲击响应。从系统建模、匹配设计、半实物试验、空投适应性4个方面进行评估,综述现有研究应用的理论、方法和研究... 系统建模仿真作为空降车辆着陆缓冲研究的重要手段,用于仿真着陆缓冲阶段的气囊排气压缩、车辆缓冲过载、姿态变化及结构冲击响应。从系统建模、匹配设计、半实物试验、空投适应性4个方面进行评估,综述现有研究应用的理论、方法和研究结论。对目前仿真模型求解效率,结构应力和气囊仿真准确度,车辆与气囊参数匹配,半实物试验,空投适应性评估等问题进行分析总结并提出进一步的研究方向。 展开更多
关键词 空降车辆 系统建模仿真 参数匹配 模型修正 空投适应性评估
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Simulation and optimization for airdrop adaptability of overweight equipment 被引量:1
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作者 徐健 李强 杨臻 《Journal of Measurement Science and Instrumentation》 CAS CSCD 2015年第3期247-252,共6页
Airbag buffer process was analyzed with the aid of aerodynamic and thermodynamic methods.Based on the current structure of the airbag,the terminal velocity was too high.Therefore,the research on the diameter and heigh... Airbag buffer process was analyzed with the aid of aerodynamic and thermodynamic methods.Based on the current structure of the airbag,the terminal velocity was too high.Therefore,the research on the diameter and height of the airbag was done and the feasible design area was found.With the optimized structure parameters,the airbag buffer experiment under normal conditions was conducted.Furthermore,the residual height and internal pressure of the airbag as well as the terminal velocity and acceleration of the airdrop were obtained.The experiment results show that the optimized airbag is feasible for 20 t cargo airdrop. 展开更多
关键词 airdrop adaptability AIRBAG terminal velocity
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