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小型飞行器跟踪地面运动目标技术研究 被引量:6
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作者 张京娟 徐烨锋 刘伟 《弹箭与制导学报》 CSCD 北大核心 2005年第SC期664-666,共3页
为提高跟踪与探测的能力.研究了利用小型飞行器对地面低速运动目标的跟踪技术。通过对初始盘旋半径、初始盘旋位置以及飞机倾斜角这几个参数之间关系的分析与仿真,表明随初始相对位置的不同,最小初始盘旋半径取值在200m~500m之间不等,... 为提高跟踪与探测的能力.研究了利用小型飞行器对地面低速运动目标的跟踪技术。通过对初始盘旋半径、初始盘旋位置以及飞机倾斜角这几个参数之间关系的分析与仿真,表明随初始相对位置的不同,最小初始盘旋半径取值在200m~500m之间不等,飞机的倾斜角就能保持在30°以下,从而有效地实现对运动目标的实时贴近跟踪与探测,仿真结果对实际系统的应用具有重要的参考价值。 展开更多
关键词 目标跟踪 活动目标探测 MAV 盘旋半径
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翼伞测控系统的设计与实验
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作者 王松松 赵敏 李宇辉 《机械制造与自动化》 2021年第2期227-229,共3页
为了能够有效地控制翼伞的飞行状态并获取翼伞飞行时的相关参数,设计一套翼伞空投测控系统,基于该系统进行了实地的空投实验。通过分析空投实验获取的有效数据,得到翼伞的实际飞行轨迹、左右操纵绳的下拉量、操纵绳的受力大小等结果。... 为了能够有效地控制翼伞的飞行状态并获取翼伞飞行时的相关参数,设计一套翼伞空投测控系统,基于该系统进行了实地的空投实验。通过分析空投实验获取的有效数据,得到翼伞的实际飞行轨迹、左右操纵绳的下拉量、操纵绳的受力大小等结果。基于上述实验结果,计算出翼伞的盘旋半径以及实际飞行时的滑降比大小。 展开更多
关键词 翼伞空投 测控系统 飞行轨迹 盘旋半径 滑降比
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Fluid flow and heat transfer characteristics of spiral coiled tube: Effects of Reynolds number and curvature ratio 被引量:5
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作者 YOO Geun-jong CHOI Hoon-ki DONG Wa-ryong 《Journal of Central South University》 SCIE EI CAS 2012年第2期471-476,共6页
Numerical analysis was performed to investigate flow and heat transfer characteristics in spiral coiled tube heat exchanger. Radius of curvature of the spiral coiled tube was gradually increased as total rotating angl... Numerical analysis was performed to investigate flow and heat transfer characteristics in spiral coiled tube heat exchanger. Radius of curvature of the spiral coiled tube was gradually increased as total rotating angle reached 12n. As the varying radius of curvature became a dominant flow parameter, three-dimensional flow analysis was performed to this flow together with different Reynolds numbers while constant wall heat flux condition was set in thermal field. From the analysis, centrifugal force due to curvature effect is found to have significant role in behavior of pressure drop and heat transfer. The centrifugal force enhances pressure drop and heat transfer to have generally higher values in the spiral coiled tube than those in the straight tube. Even then, friction factor and Nusselt number are found to follow the proportionality with square root of the Dean number. Individual effect of flow parameters of Reynolds number and curvature ratio was investigated and effect of Reynolds number is found to be stronger than that of curvature effect. 展开更多
关键词 spiral coiled tube heat exchanger Reynolds number curvature ratio secondary flow friction factor Nusselt number
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Characteristics of Transient Vortices in the Boundary Layer on a Rotating Disk under Orbital Motion
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作者 Mizue Munekata Naoya Jobi +1 位作者 Keiichiro Kubo Hiroyuki Yoshikawa 《Journal of Thermal Science》 SCIE EI CAS CSCD 2013年第6期600-605,共6页
The objective of this study is to experimentally examine the characteristics of transient vortices in the boundary layer on a disk undergoing both rotation and orbital motion. The velocity fluctuations on a rotating, ... The objective of this study is to experimentally examine the characteristics of transient vortices in the boundary layer on a disk undergoing both rotation and orbital motion. The velocity fluctuations on a rotating, orbiting disk (disk radius equal to orbital radius) are measured by the hot-wire method, and the effects of orbital motion on the transient vortices in the boundary layer are examined. When the ratio of the orbital speed to the speed of rotation is i-0.025, the interval of transient vortices depends on only the orbital radius, regardless of the directions of rota- tion and orbital motion. The rate of low-frequency disturbances increases as the orbital speed increases, and the vortices induced by these low-frequency disturbances travel over the disk and then develop in the region of in- creased velocity. Consequently, no vortices generated on a rotating disk under orbital motion are stationary rela- tive to the disk. 展开更多
关键词 Boundary layer transition Transient vortex Rotating disk Velocity measurement Hot-wire ane-mometer
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