微型飞行器的英文

• micro air vehicle

• "微型"英文翻译    miniature; minitype; mini-
• "飞行器"英文翻译    aerobat; air vehicle; beast; ...
• "微型飞行机器人" 英文翻译 :    micro flying robot
• "微型飞机" 英文翻译 :    diminutive airlane
• "飞行器" 英文翻译 :    aerobat; air vehicle; beast; bird; flight vehicle
• "恒压型飞行" 英文翻译 :    constant-pressure-pattern flight; constant-pressuro pattern flight
• "气流型飞行" 英文翻译 :    wind pattern flying
• "气压型飞行" 英文翻译 :    pressure pattern flight; pressure pattern flying; pressure-pattern flying
• "摆渡飞行器" 英文翻译 :    ferrycraft
• "成象飞行器" 英文翻译 :    imaging se ors; imaging sensors
• "待命飞行器" 英文翻译 :    aircraft prepared for service (aps)
• "单人飞行器" 英文翻译 :    individual lift device
• "低空飞行器" 英文翻译 :    low flyer
• "地效飞行器" 英文翻译 :    ground effect vehicle
• "调用飞行器" 英文翻译 :    have jetpack
• "渡运飞行器" 英文翻译 :    ferrycraft
• "发射飞行器" 英文翻译 :    launch craft
• "飞行器测试" 英文翻译 :    aircraft_testing
• "飞行器定向" 英文翻译 :    vehicle organization
• "飞行器结构" 英文翻译 :    flight construction; flight-vehicle structure
• "飞行器列表" 英文翻译 :    list of aircraft
• "飞行器螺旋" 英文翻译 :    vehicle spin
• "飞行器模拟" 英文翻译 :    aircraft simulation
• "飞行器能量" 英文翻译 :    vehicle energy
• "飞行器裙部" 英文翻译 :    vehicle skirt

• Experimental investigation of aerodynamic configuration for mavs
  微型飞行器相关布局气动特性实验研究
• Miniature wireless data communication system for micro air vehicles
  微型飞行器的微型无线数据传输系统
• Attitude tracking control for flapping wing micro aerial vehicle based on feedback compensation
  基于反馈补偿的扑翼微型飞行器姿态跟踪控制
• The bionic flying micro - robot is a complicated intelligent robot , i . e . and a micro aerial vehicle
  摘要微型仿生扑翼飞行器是一种新概念的微型飞行器。
• According the need of micro craft , a test system was presented which can implement the driving of rotor , set parameters and testing
  文章根据微型飞行器的系统需求，设计并完成了一套可以实现旋翼驱动和上层计算机参数设置和控制的测试系统。
• Particularly the navigation system is analyzed in detail in the above discussion . later an autonomous flight control system is designed for a mini unmanned aerial vehicle
  接着在此基础上讨论了微型飞行器的自主导航系统，研究采用传统的飞控理论和模糊控制理论来实现自主控制系统。
• Combined with blade element theory , the results can be used to evaluate aerodynamic characteristics of flapping wings , which are helpful for the initial design of micro rotary and flapping wing
  运用本文方法分析了各参数对翼型气动特性的影响，进一步结合叶素理论还可以估算扑翼的气动特性，进而指导微旋翼或扑翼微型飞行器的初期设计。
• In this paper micro aerial vehicles are introduced . on the base of the detail discussion of the applications of sensors and components of mav , several schemes of autonomous flight control system are presented
  本文先简单介绍了微型飞行器的发展概况，然后阐述微型飞行器的系统结构和气动特性，接着详细讨论微型器件，特别是传感器对微型飞行器的重要性及其应用。
• This paper uses above - mentioned methods to design double - wing mav aerodynamic shapes with normal and robust optimization . results shows robust optimization shapes lost some aerodynamic performance but become more steady
  本文采用上述基于代理模型的稳健优化方法对微型飞行器气动外形进行确定性和稳健优化设计,所得结果显示稳健优化结果虽然损失了一些气动性能,但其气动特性变得更加稳健。
• In this paper , fuzzy logic theory is discussed in order to find a better control project for may so first , we should carry through this experiment to acquisite a lot of data which help to create a fuzzy model . second , we should draw a conclusion from so much data
  整个系统采用c语言进行程序设计，很大程度上增加了系统的适应性与灵活性。最后，进行了总结，对微型飞行器飞控系统理论的发展提出个人的一些看法和观点。