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   飞行器 在 航空航天科学与工程 分类中 的翻译结果: 查询用时:0.062秒
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飞行器     
相关语句
  aircraft
    Reliability Analysis and Optimization Design of Aircraft Structure
    飞行器结构可靠性分析与优化设计研究
短句来源
    AERODYNAMIC COEFFICIENT IDENTIFICATION OF TIME-VARYING AIRCRAFT SYSTEM AND ITS APPLICATION
    变系数飞行器系统气动系数辨识计算与应用
短句来源
    ADVANCES IN IDENTIFICATION OF AIRCRAFT AERODYNAMIC PARAMETERS
    飞行器气动参数辨识进展
短句来源
    A VARIABLE STRUCTURE SYSTEM(VSS) TO ROBUST CONTROL OF AIRCRAFT
    飞行器变结构鲁棒控制
短句来源
    AN IDENTIFICATION METHOD OF FAST TIME VARYING PARAMETERS ADAPTED TO AIRCRAFT CONTROL SYSTEMS
    一种适用于飞行器控制系统的快速时变参数辨识方法
短句来源
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  vehicle
    Research on Airframe/Engine Integration Issues and Multidisciplinary Design Optimization Methods for Airbreathing Hypersonic Vehicle
    高超声速飞行器机体/发动机一体化及总体多学科设计优化方法研究
短句来源
    Error Modeling of MEMS Gyroscopes and Its Application on Flight Vehicle Integrated Navigation
    微机电陀螺误差建模及其在飞行器组合导航中的应用
短句来源
    THE OPTIMIZATION DESIGN OF EARTH ORBIT REENTRY VEHICLE CONFIGURATIONS FOR MINIMUM AERODYNAMIC HEAT TRANSFER
    地球轨道再人飞行器最小气动加热外形优化设计
短句来源
    A STUDY OF ACTIVE VEHICLE STRUCTURE VIBRATION AND DECOUPLING WITH CONTROL SYSTEM AS WELL AS INITIATIVE SUPPRESSION
    飞行器结构振动和控制系统解耦及主动抑制的研究
短句来源
    HYBRID GUIDANCE ABOUT MANEUVERING FLIGHT VEHICLE
    机动飞行器的混合制导
短句来源
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  spacecraft
    LARGE ANGLE ATTITUDE MANEUVERS AND CONTROLS OF GYROSTAT SPACECRAFT
    陀螺体飞行器大角度姿态机动与控制
短句来源
    OPTICAL MEASUREMENT OF POSITION AND ATTITUDE FOR TARGET SPACECRAFT
    目标飞行器位置姿态的光学测量
短句来源
    VARIABLE-STRUCTURE CONTROL OF LIQUID-FILLED SPACECRAFT LARGE-ANGLE MANEUVERS
    充液飞行器大角度操纵变结构控制
短句来源
    The Kalman Filtering Estimation of Determining a Spacecraft Attithde by Measuring Starlight
    通过星光测量确定飞行器姿态的Kalman滤波估计
短句来源
    Imtegrated Application of Information of GPS and Inertial Guidance in the Spacecraft Guidance
    GPS和惯导信息在飞行器制导中的综合应用
短句来源
更多       
  flight vehicle
    Error Modeling of MEMS Gyroscopes and Its Application on Flight Vehicle Integrated Navigation
    微机电陀螺误差建模及其在飞行器组合导航中的应用
短句来源
    HYBRID GUIDANCE ABOUT MANEUVERING FLIGHT VEHICLE
    机动飞行器的混合制导
短句来源
    Development and Application of a Flight Vehicle Automatic Testing System Based on VXI Bus
    基于VXI总线的某型飞行器自动测控系统研制与应用
短句来源
    ARTIFICIAL INTELLIGENCE ANALYSIS AND DIAGNOSIS OF FLIGHT VEHICLE VIBRATION
    飞行器振动智能分析与诊断
短句来源
    Neural Network for Estimating the Main Parameters in Flight Vehicle Preliminary Design
    飞行器总体设计中主要参数的神经网络估算
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  aircraft
The Use of Micromycetes for Cleaning Parts of Aircraft Engines
      
These fungi actively destruct carbon deposits formed during operation of aircraft.
      
A biotechnological method for removing fouling from parts of aircraft engines (PAE) was developed.
      
The solution was illustrated by an instructional example and an example of control of the aircraft lateral (roll-yaw) motion.
      
An approach to designing algorithms for confining constraints within the aircraft control trajectory is elaborated on the basis of geometric transformations in three-dimensional state space.
      
更多          
  vehicle
Implementation of an OFDM underwater acoustic communication system on an underwater vehicle with multiprocessor structure
      
Experimental Research on Friction of Vehicle Tire Rubber
      
The prediction technology study of fatigue life for key parts of a tracked vehicle's suspension system
      
In allusion to fatigue life of a tracked vehicle torsion bar, a virtual prototype model of the tracked vehicle suspension system including a flexible torsion bar was built based on dynamic simulation software-ADAMS.
      
The finite element analysis of the vehicle frame was made and the result satisfied the requirements.
      
更多          
  spacecraft
This collection can be used to test spacecraft production materials, in order to determine their resistance to biodegradation.
      
Studying Stability of the Flexible Spacecraft with a Discrete Control System
      
Stability of the spacecraft was considered with regard for its elastic structural oscillations arising under discrete control.
      
Consideration was given to the possibility of estimating jointly the motion coordinates and parameters of the elastic spacecraft using algorithms based on the discrete Kalman filtering and the theory of testing statistical hypotheses.
      
Design of the Suboptimal Profiled Relay Control of Orientation of the Spacecraft Having Elastic Structural Elements with Regard
      
更多          
  flight vehicle
Some problems of flight vehicle control that date back to the 1950s and gave rise to the theory of adaptive control and, in the 1960s and 1970s, self-adjusting automatic pilots were discussed.
      
The variational problem of determining the optimal contour of an outlet system consisting of the supersonic jet-engine nozzle and the tail of the flight vehicle is solved by the direct method.
      
Design of the optimal nozzle of a hypersonic flight vehicle for given overall dimensions and moment
      
The lift of the flight vehicle is treated as the optimized functional.
      
Distinctive Features of the Flow past a Flight Vehicle Integrated with an Air-Breathing Engine at High Supersonic Velocities
      
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