aerocraft
美 ['eərəkræft] 
英 ['eərəkrɑ:ft]
同义词
英汉解释
例句
Data bus technology is a means of communication widely used in aerocraft control system.
数据总线技术是飞行器控制系统中广泛采用的一种通讯方式。
Finally, it was applied in the fault diagnosis for aerocraft and the result of experiments is satisfactory.
将其应用在飞行器故障诊断中，取得了很好的效果。
The method that uses optical correlation recognition in landing site tracking is proposed to achieve the aerocraft precise landing.
提出将光学相关识别应用于着陆点的选择中，以解决飞行器精确定点着陆问题。
The paper introduces the launch modes and characteristics of the high speed and low speed near space aerocraft.
介绍了高速临近空间飞行器和低速临近空间飞行器的发射方式和特点。
As the control center of aerocraft, it is necessary to ensure the high reliability of controller design.
控制器是航天飞行器的控制中枢，必须确保其高可靠性设计。
The propellant metal diaphragm tanks are important component of drive system of aerocraft.
推进剂金属膜片贮箱是空间飞行器上主要的驱动系统。
The result also shows considering the effect of the deformation of elastic aerocraft which is in the maneuvering flight is very necessary.
这对于飞行器纵向气动操纵特性会产生较大影响，同时也说明在大机动飞行过程中计入飞行器的弹性变形是非常必要的。
The paper mainly studies on the technology of speech command recognition based on aerocraft in the aerial domain.
本课题主要研究在航空领域中飞行器语音指令识别技术。
The study provide a theoretical basis for the design of the micro aerocraft and development of the self cleaning material.
蜻蜓翅膀润湿性能的研究为微型飞行器及自清洁材料的制备提供了理论依据。
By using the method, it can effectively analyse the aerocraft Simulate Training System's failure.
将此方法运用到飞行器模拟训练系统中可有效地对该系统进行故障分析。
Experimental Research on the Flexible Wing and Its Theoretical Explanation for the Bionics Flapping Aerocraft
仿生扑翼飞行机器人柔性翅试验研究及其理论解释
The Design Study of Variable Structure Attitude Control of Large Angle Maneuverable Aerocraft
大角度机动飞行器变结构姿态控制设计研究
Distilling character parameter method investigation for space aerocraft propulsion system using improving time-series method
利用改进时序模型提取空间推进系统特征参数
Variable Structure Control for High Speed Reentry Aerocraft and Its Simulation Studies
高速再入飞行器的变结构控制及其六自由度仿真研究
A Research of the Technique of Optimizing the Orbit-alteration for the Exact-landing of Aerocraft by Using Evolution-algorithm
基于进化算法的在轨对地定点着陆优化变轨分离技术
Physical modeling of aerocraft frame part with different shape transverse section during isotherm deformation
不同截面形状结构件等温成形规律的物理模拟
The Design and Realization of a Type Aerocraft Pitot-Static Pressure System
某型飞行器全静压检测系统的设计实现
Thermo-structural experiment coupling of aero-heating environment and structural response of aerocraft
飞行器气动加热环境与结构响应耦合的热结构试验方法
Identification of Aerodynamic Parameters of an Aerocraft
飞行器气动力参数辨识
Analysis Techniques for Aerocraft Mechanism Reliability and Application
飞行器机构可靠性分析技术及应用
Heating Research on Driven Motor Used in Wind Tunnel Test of Propeller Aerocraft Model
螺旋桨飞机模型风洞实验驱动电机发热研究
Fuzzy Sets and Research of the Hybrid Fault Tree Analysis and the Application in the Aerocraft Simulate Training System
模糊集与故障树复合分析法研究及其在飞行器模拟训练系统中的应用
Simulation of Target Air Capture Probability of Aerocraft Terminal Guidance for Long-Distance Attack
远程攻击末制导目标截获概率数字仿真
Project algorithm of the electromagnetic scatter of the aerocraft cavity and cabin
飞行器腔舱结构电磁散射的一种工程算法
Application on Data of Aerocraft Inertial Navigation System in Measurement and Control System
飞行器惯导数据在海上靶场测控中的应用
The Technology of Remote-Control Programming for Aerocraft Embedded Software
一种基于飞行器平台的嵌入式软件重构技术
The Research of Model on Aerial Defence Missile Weapon System Detecting and Firing Low-height Aerocraft
防空导弹武器系统探测拦截低空飞行器模型
Robust adaptive fuzzy decoupling control for the attitude of aerocraft
飞行器姿态的一种鲁棒自适应模糊解耦控制
The Evaluation of a Aerocraft Datarecorder's Reliable Increase
基于某飞行器数据记录器的可靠性增长的评估
Research on Aerocraft Shape Design System with Knowledge Based Engineering
基于知识的飞行器外形设计系统研究
Influence of Launching Origin Location Error on Precision of Aerocraft Orbit Solving
发射点定位误差对飞行器轨道融合解算精度的影响
An Independent Design Method for Three Channels of Aerocraft Attitude Control
一种飞行器姿态控制的三通道独立设计方法
Information Transmitted between Levels of Multilayer Buses System of Aerocraft
飞行器多层总线系统级间信息的传输
Research on Model and Simulation of an Aerocraft Rudder Loop
飞行器舵回路仿真研究及试验分析
Key Technologies of Developing Near Space Aerocraft Systems
发展近空间飞行器系统的关键技术
Research on Accurate Test of Motion Parameter of the Aerocraft
某飞行器运动参数精密检测研究
Status and prospects of driving mode about the wing for the bionics flapping aerocraft
仿生扑翼飞行器翅翼驱动方式的研究现状及展望
A Method for Improving on Measure Data Precision of Spaceflight Aerocraft
提高航天飞行器外测数据精度的处理方法
Research and analysis on material and machining for aerocraft engine gear
航空发动机齿轮材料及加工精度分析研究
Design for aerocraft attitude control system based on feedback-linearization and variable-structure-control
基于反馈线性化和变结构控制的飞行器姿态控制系统设计
