飞行特性的英文

• flight characteristics
• flight efficiency
• flight performance
• flying characteristics

• "飞行"英文翻译    flight; flying; aviate; voya ...
• "特性"英文翻译    characteristic; character; p ...
• "垂直飞行特性" 英文翻译 :    vertical-flight characteristics
• "单发飞行特性" 英文翻译 :    single-engine flight characteristics
• "导弹飞行特性" 英文翻译 :    missile-flight data
• "低速飞行特性" 英文翻译 :    low-speed characteristics
• "飞机飞行特性" 英文翻译 :    aircraft nisht
• "飞行特性试验" 英文翻译 :    flight characteristics test
• "高速飞行特性" 英文翻译 :    high-speed characteristics
• "仪表飞行特性" 英文翻译 :    instrument flight characteristics
• "自由飞行特性" 英文翻译 :    free-flight characteristics
• "低亚音速飞行特性" 英文翻译 :    low-subsonic characteristics
• "高超音速飞行特性" 英文翻译 :    high-supersonic characteristics
• "极高速飞行特性" 英文翻译 :    hypervelocity characteristics
• "小速度飞行特性" 英文翻译 :    slow-flight characteristics
• "直升机下降飞行特性" 英文翻译 :    helicopter descent characteristics
• "滑行特性" 英文翻译 :    taxiing characteristics
• "仅执行特性" 英文翻译 :    execute only attribute
• "漂行特性" 英文翻译 :    floating characteristics
• "运行特性" 英文翻译 :    in-service behavior; operating characteristics; operational characteristic; performance characteristics; roadability; running characteristic; running performance; service performance
• "飞行特技" 英文翻译 :    acrobatic feat; aerial aerobatics; aerobation
• "并行特性编码" 英文翻译 :    parallel attribute coding
• "车辆运行特性" 英文翻译 :    running qualities of a wagon
• "电机运行特性" 英文翻译 :    electric machine operating characteristic
• "短程航行特性" 英文翻译 :    short-range trip response

• Utilize data processing method , two groups of data of the towed plane is compared
  利用数据拟合方法，对计算数据进行比较，分析牵引飞行特性。
• The composite grips extend bearing life , while working with the innovative two - stage dampening to give the n9 incredible flight characteristics
  综合枪柄轴承延长寿命,同时与创意两阶段调高给n9不可思议的飞行特性
• Here , active means defined shifts in load take place during the flight manoeuvre in order to investigate the flying characteristics
  在这里，实际模拟就是在为了研究飞行特性而进行的飞行演习中，所产生的力的变化情况。
• Therefore it can influence the fidelity and variety of flight training , and is one of the important criteria for determining whether a flight simulator is advanced
  航空仪表系统作为飞行模拟器中的重要组成部分,提供给飞行员关于飞机状态和飞行特性等相关信息。
• Not only does the photo show a flying saucer , but the flight characteristics described by the witness defy conventional aerial motion because the object was moving rapidly , stopped , hovered , and then sped off
  不仅图片表现出飞碟,但飞行特性描述的证人藐视常规空中议案,是因为物体移动快,停,盘旋,然后迅速赶过
• In order to study the flight characteristics and control rules in taking off and landing period better to promote flight safety of uav in this stage , we started the study of take off and landing simulation system research of uav based on a certain type of uav
  为更好地研究无人机在起飞、着陆阶段的飞行特性,控制规律,以保证无人机在这一阶段的飞行安全,我们以某型无人机为对象进行无人机的起飞、着陆仿真系统研究。
• Through calculating and analyzing basic performance , the flight characteristic of the towed system is researched . stability and control issue of carrier rocket is discussed primarily . the net result of the thesis will prove the feasibility of the scheme of towed launch
  论文通过牵引系统基本性能的计算和分析，完成牵引飞行特性的研究，同时对运载器的稳定性和控制问题进行初步的探讨，最终结果将验证牵引发射方案的可行性。
• Based on the aerodynamic characteristics of space shuttle booster - like missile bodies at angle of attack from 0 to 180 , the flying characteristics of high maneuver at 90 angle of attack and velocity consuming at 180 angle of attack are analyzed
  摘要以新一代无翼式气动布局导弹为背景，在大攻角气动特性理论基础上，分析了在导弹主动段、攻角在180范围内变化的导弹飞行特性，得出了90内大攻角最大转弯能力和180攻角附近最大降速效果的结论。
• 5 ) . using tools of animation . according to flying pose of armor piercing projectile and data from experiment , actually animate the track of ballistics whole procedure . lt can dynamically simulate to obtain visual scientific calculation and accurate simulation in real meaning
  5 )利用图像仿真工具，根据脱壳穿甲弹的飞行特性以及计算和试验获得的数据，对脱壳穿甲弹全弹道飞行特性进行仿真，比较真实地反映脱壳穿甲弹全弹道的飞行特性，实现了科学计算可视化的要求。
• The modern unmanned helicopter flight control system is generally composed of the flight control computer , the servo driving mechanism , the sensor , and the ground monitor control system etc . in this thesis the research to the helicopter flight characteristics was conducted at first , and its flight dynamic model was preliminary discussed , especially the mathematic model under hung - stop condition was formulated and the algorithm of the controller was designed in detail
  现代无人直升机飞行控制系统一般由飞行控制计算机、伺服驱动机构、传感器、地面监测控制等分系统组成。本文首先对直升机的飞行特性进行了研究,并且对飞行动力数学模型做了初步探讨,尤其对在悬停状态下的数学模型做了较为详尽的公式推导和控制器的算法设计。