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Investigation of Key Parameters for 3-D Dredging Plume Model Validation
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作者 Junsheng Jiang 《Journal of Shipping and Ocean Engineering》 2014年第5期129-139,共11页
Dredging plume dispersion studies, use dredging plume models to predict the fate of sediment plumes resulting from dredging activities and dredge spoil disposal. The model results are applied as input to environmental... Dredging plume dispersion studies, use dredging plume models to predict the fate of sediment plumes resulting from dredging activities and dredge spoil disposal. The model results are applied as input to environmental impact assessment of the proposed dredging, particularly those associated with suspended sediments and sedimentation. Model validation and performance are still not resolved because of the difficulty of site measurements and the understanding of the parameters used in the model. This paper presents a 3-D dredging plume model based on the MIKE3 software package to investigate parameters which affect the model performances. As a result of lack of site data for the public domain uses, the model scenarios are designed artificially for sensitive runs to identify the key parameters affecting plume behaviours. The factors include dredging spill rates using different dredging methods, equipment and sediment settling velocities. The influence of wave and wind effects combined with tidal forces on the sediment re-suspended rates and the advection/dispersion scales are also assessed. 展开更多
关键词 3-d dredging plume model settling velocity sediment measurement.
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Three-dimensional finite-time cooperative guidance for multiple missiles without radial velocity measurements 被引量:22
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作者 Teng LYU Chuanjiang LI +1 位作者 Yanning GUO Guangfu MA 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第5期1294-1304,共11页
In order to simultaneously attack a target with impact angle constraint in threedimensional(3-D) space, a novel distributed cooperative guidance law for multiple missiles under directed communication topologies is pro... In order to simultaneously attack a target with impact angle constraint in threedimensional(3-D) space, a novel distributed cooperative guidance law for multiple missiles under directed communication topologies is proposed without radial velocity measurements. First, based on missiles-target 3-D relative motion equations, the multiple missiles cooperative guidance model with impact angle constraint is constructed. Then, in Line-of-Sight(LOS) direction, based on multiagent system cooperative control theory, one guidance law with directed topologies is designed with strict proof, which can guarantee finite time consensus of multiple missiles' impact times. Next, in elevation direction and azimuth direction of LOS, based on homogeneous system stability theory and integral sliding mode control theory, two guidance laws are proposed respectively with strict proof, which can guarantee LOS angles converge to desired values and LOS angular rates converge to zero in finite time. Finally, the effectiveness of the designed cooperative guidance law is demonstrated through simulation results. 展开更多
关键词 3-d cooperative guidance Directed communication TOPOLOGIES FINITE time Impact angle CONSTRAINT RADIAL velocity measurementS
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基于飞蛾触角的仿生MEMS导航传感器的设计与仿真 被引量:2
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作者 唐军 刘尧 +5 位作者 刘俊 郭浩 石云波 张贺 温涣飞 赵锐 《传感技术学报》 CAS CSCD 北大核心 2012年第5期561-565,共5页
以飞蛾触角导航为仿生依据,通过建立其导航数学模型,利用MATLAB对该模型的导航原理进行仿真分析,结合仿生学,设计了一种新型MEMS三维角速度传感器模型,并对该传感器的加工工艺进行了设计,该传感器主要由折叠梁和坡莫合金棒组成,通过ANSY... 以飞蛾触角导航为仿生依据,通过建立其导航数学模型,利用MATLAB对该模型的导航原理进行仿真分析,结合仿生学,设计了一种新型MEMS三维角速度传感器模型,并对该传感器的加工工艺进行了设计,该传感器主要由折叠梁和坡莫合金棒组成,通过ANSYS分析,在9 V驱动电压的作用下,合金棒沿X、Y的振动幅度可达到80μm,通过理论计算,由偏航角速度产生的哥氏力为0.908×10-8N/(°·s-1),由翻滚和俯仰角速度产生的哥氏力为0.18×10-9N/(°·s-1)。 展开更多
关键词 仿生MEMS 三维角速度传感器 有限元分析 飞蛾触角
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基于蜜蜂平衡棒的仿生MEMS导航传感器的设计与仿真 被引量:2
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作者 刘尧 唐军 +1 位作者 刘俊 曹卫达 《传感技术学报》 CAS CSCD 北大核心 2012年第10期1395-1399,共5页
针对目前角速度传感器检测维数单一、体积大的缺点,以蜜蜂平衡棒为仿生模型,详细分析了平衡棒的导航原理,结合MEMS技术,设计了一种新型的三维角速度微传感器。利用ANSYS对传感器结构进行仿真、优化,得到了合适的结构尺寸,在±20 V... 针对目前角速度传感器检测维数单一、体积大的缺点,以蜜蜂平衡棒为仿生模型,详细分析了平衡棒的导航原理,结合MEMS技术,设计了一种新型的三维角速度微传感器。利用ANSYS对传感器结构进行仿真、优化,得到了合适的结构尺寸,在±20 V的驱动电压下,传感器结构中的微柱体摆动幅度可达到7.04°,通过进一步理论计算得到翻滚、俯仰角速度产生的哥氏力为2.467×10-5N/(°.s-1),偏航角速度产生的哥氏力为7.58×10-7N/(°.s-1)。 展开更多
关键词 仿生MEMS 三维角速度传感器 有限元分析 蜜蜂平衡棒
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