The Comparing Method between Tracking and Telemetry of Flying Height above Sea Level for Missile Measures to Improving up to grade Rate of Telemetering Estimating in Weihai Power System 导弹掠海飞行高度遥、外测比对方法威海电网提高遥测估计合格率的方法
The aircraft was flying at a height of 2000 feet. 飞机在2000英尺的高空飞行。
We'll be flying at a height of80000 meters. 我们将在8万米高空飞行。
Once gimbal got heated it bents itself toward platter's surface and this action reduces flying height. 一旦得到了热烈的万向节是本茨对盘片表面上的行动本身,这降低了飞行高度。
They set a new world record for the flying height of the powered paraglider. 他们创造了动力滑翔伞飞行高度新的世界纪录。
Aerobatic flights over airfield up to 2000m. The Comparing Method between Tracking and Telemetry of Flying Height above Sea Level for Missile 花样飞行在机场上空,高度2000米。导弹掠海飞行高度遥、外测比对方法
Its flying height was343 kilometers. 它的高度是343千米。
The heater can help adjust heads flying height. 加热器可以帮助调整飞行高度负责。
The plane is flying at a height of10000 metres. 飞机正在10000米的高空飞行。
In modern times the flying height of the cruise missile is below 30 meters. 现代飞航导弹的巡航高度一般都低于30米,进行掠海飞行。
So in the practical application, the laser beam's wavelength should be chosen according to the different flying height of the aircraft. 因而在实际应用时,应该根据飞行器所处的不同飞行位置合理选择驱动光波长。
In flying height measuring method utilizing light intensity interference principle, the position control of micro flying head has effect on measuring error. 基于强度干涉原理的飞高检测方案中,微型飞行头位姿控制是影响测量误差的一项关键因素。
The results indicate: with the increasing the flying height and scanning angle, the received backscattered power decreases rapidly, the SNR deteriorates seriously and the ranging error increases significantly. 计算表明,随航高和扫描角度的增加,回波信号功率衰减,信噪比降低,测距误差增大。
Study of Deep Sub-micron Flying Height Measuring Technology 深亚微米飞行高度测量技术研究
The course of take-off and landing are both divided into three phases: The phase from flying at safe height to contacting the ground. 本论文把起飞和着陆过程均分为三个阶段:从安全高度到接触地面阶段。
Thoughts of Basic Slipping and Flying Height in the Half Pipe Eternal Height The Flying Box 对U型场地单板雪上技巧项目基础滑行和飞起高度的思考
According to the analysis of the flying height requirement of super high-density recording, it is necessary to take the rough into consideration. 根据对超高密度记录浮动间距要求的分析,必须考虑粗糙度的影响。
Design of Optoelectronic Detection System for Deep Sub-micron Flying Height Measuring 深亚微米飞高测量的光电检测系统设计
Within the field of ground effect, aerodynamic forces of the wing in surface effect crafts are not only decided by the angle of attack, but also by the flying height, and they lead to more complicated stability problems. 在地效作用区域内,地效飞机的气动力不仅与迎角有关,而且与飞行高度有关,因而其飞行稳定性问题更为复杂。
A Study on Magnetic Head Slider witt Constant Flying Height 等飞高磁头的研究
Based on the optoelectronic sense principle, a set of optoelectronic detection system for deep sub-micron flying height measuring is designed, which focuses on the preamplifier and post amplifier. It is a high-speed and high-precision data acquisition system, and the system control interactive interface is introduced. 基于光电传感原理,设计了用于深亚微米飞高测量的光电检测系统,采用前置放大和后级放大电路结合,设计高速高精度数据采集系统,介绍了系统控制交互界面。
Analysis and experiment show that this system has proper parameters on linearity of optoelectronic detection system, measuring resolution and dynamic frequency, and can realize dynamic measuring for the deep sub-micron flying height. 性能测试结果表明,该光电检测系统线性度、分辨率和动态频率均满足飞高动态测试的要求。
The each Co nanowire represented a single domain structure. The distribution of domain was corresponded to its morphology properties. The size of domain changed a little with the flying height of the magnetic tip. 结果表明,纳米磁记录阵列膜里的每一根Co纳米线均为单畴结构,磁畴分布非常有序且与氧化铝微孔的形貌分布一一对应,畴的大小随磁力针尖离样品的高度不同略有变化;
Flying Height Control of Solid Immersion Lens by Slipstream 固体浸没透镜飞行高度的气浮控制
But, as the increase of airplane flying speed and height and the enhancement of maneuverability, the impact on aeroengine by inlet distortion is more and more prominent. 但随着飞机飞行速度、高度的不断提高,机动性的不断增加,以及导弹武器的使用,畸变的影响越来越突出,实践中暴露出来的问题也越来越严重。
Effective environmental model is built in the case of UAV flying at a constant height. 根据无人机定高飞行,建立了合适的环境模型。
But to use SIL recording, the problems of the focusing servo and the dynamically flying height control of the SIL must be solved. 但是,固体浸没透镜光存储系统必须解决精密聚焦伺服问题和动态飞行高度控制问题。
The simulation results will provide a theoretical guide to the actual design of the flying height control slider. 仿真结果为指导实际热飞高控制滑块系统设计提供了理论依据。