目的研究舰载系留气球在海洋环境下对系留缆绳以及球体姿态的影响。方法采用ADAMS二次开发宏命令来建立离散化系留缆绳模型,并将离散化系留缆绳几何模型在相邻微段圆柱间添加Bushing轴套力,设置相关刚性系数和阻尼系数获得完整特效的缆...目的研究舰载系留气球在海洋环境下对系留缆绳以及球体姿态的影响。方法采用ADAMS二次开发宏命令来建立离散化系留缆绳模型,并将离散化系留缆绳几何模型在相邻微段圆柱间添加Bushing轴套力,设置相关刚性系数和阻尼系数获得完整特效的缆绳模型。同时根据船用起重机的相关设计规范,考虑船体横摇5°和纵摇2°等运动影响,分析船体运动情况可知,纵摇时系留缆绳下端系固点位置较之横摇波动幅度更大,对缆绳的影响更大,因此主要研究船体纵摇2°情况下对于系留缆绳的影响,并分析对比船体静止以及船体纵摇2°情况下对于舰载系留气球系留缆绳以及球体姿态的影响。结果获得了在船体静止状态以及纵摇激励影响下舰载系留气球系留缆绳张力变化曲线以及球体姿态变化曲线。船体纵摇2°情况时,系留缆绳在仿真开始阶段承受冲击载荷较大,峰值达到150 kN,随后缆绳载荷基本在25 k N上下浮动。张力变化曲线整体呈现周期变化,周期与船体纵摇周期一致,为10 s。球体横滚角和航向角变化与船体静止状下仿真结果基本一致,球体俯仰角变化幅度较大。结论船体纵摇时会对系留缆绳带来较大的冲击载荷,同时对球体的俯仰姿态产生影响。该仿真结果对舰载系留气球的可行性分析和适装性研究以及系留缆绳的选用具有较大的指导意义。展开更多
The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo m...The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo mapping camera equipped on lunar orbiter before launching.In this work,an imaging simulation method consid-ering the attitude jitter is presented.The impact analysis of different attitude jitter on terrain undulation is conduct-ed by simulating jitter at three attitude angles,respectively.The proposed simulation method is based on the rigor-ous sensor model,using the lunar digital elevation model(DEM)and orthoimage as reference data.The orbit and attitude of the lunar stereo mapping camera are simulated while considering the attitude jitter.Two-dimensional simulated stereo images are generated according to the position and attitude of the orbiter in a given orbit.Experi-mental analyses were conducted by the DEM with the simulated stereo image.The simulation imaging results demonstrate that the proposed method can ensure imaging efficiency without losing the accuracy of topographic mapping.The effect of attitude jitter on the stereo mapping accuracy of the simulated images was analyzed through a DEM comparison.展开更多
文摘目的研究舰载系留气球在海洋环境下对系留缆绳以及球体姿态的影响。方法采用ADAMS二次开发宏命令来建立离散化系留缆绳模型,并将离散化系留缆绳几何模型在相邻微段圆柱间添加Bushing轴套力,设置相关刚性系数和阻尼系数获得完整特效的缆绳模型。同时根据船用起重机的相关设计规范,考虑船体横摇5°和纵摇2°等运动影响,分析船体运动情况可知,纵摇时系留缆绳下端系固点位置较之横摇波动幅度更大,对缆绳的影响更大,因此主要研究船体纵摇2°情况下对于系留缆绳的影响,并分析对比船体静止以及船体纵摇2°情况下对于舰载系留气球系留缆绳以及球体姿态的影响。结果获得了在船体静止状态以及纵摇激励影响下舰载系留气球系留缆绳张力变化曲线以及球体姿态变化曲线。船体纵摇2°情况时,系留缆绳在仿真开始阶段承受冲击载荷较大,峰值达到150 kN,随后缆绳载荷基本在25 k N上下浮动。张力变化曲线整体呈现周期变化,周期与船体纵摇周期一致,为10 s。球体横滚角和航向角变化与船体静止状下仿真结果基本一致,球体俯仰角变化幅度较大。结论船体纵摇时会对系留缆绳带来较大的冲击载荷,同时对球体的俯仰姿态产生影响。该仿真结果对舰载系留气球的可行性分析和适装性研究以及系留缆绳的选用具有较大的指导意义。
基金Supported by the National Natural Science Foundation of China(42221002,42171432)Shanghai Municipal Science and Technology Major Project(2021SHZDZX0100)the Fundamental Research Funds for the Central Universities.
文摘The geometric accuracy of topographic mapping with high-resolution remote sensing images is inevita-bly affected by the orbiter attitude jitter.Therefore,it is necessary to conduct preliminary research on the stereo mapping camera equipped on lunar orbiter before launching.In this work,an imaging simulation method consid-ering the attitude jitter is presented.The impact analysis of different attitude jitter on terrain undulation is conduct-ed by simulating jitter at three attitude angles,respectively.The proposed simulation method is based on the rigor-ous sensor model,using the lunar digital elevation model(DEM)and orthoimage as reference data.The orbit and attitude of the lunar stereo mapping camera are simulated while considering the attitude jitter.Two-dimensional simulated stereo images are generated according to the position and attitude of the orbiter in a given orbit.Experi-mental analyses were conducted by the DEM with the simulated stereo image.The simulation imaging results demonstrate that the proposed method can ensure imaging efficiency without losing the accuracy of topographic mapping.The effect of attitude jitter on the stereo mapping accuracy of the simulated images was analyzed through a DEM comparison.
