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quality
    Helicopter Neural Network Control and Implementation of Handling Quality Requirements
    直升机神经网络控制与飞行品质要求的实现
    Reconstruction of High Quality Engineering Surfaces and Surface Interrogation
    高质量工程曲面的重建与曲面品质检查分析
    ATMOSPHERIC TURBULENCE AND FLYING QUALITY REQUIREMENTS
    大气扰动和飞行品质要求
    AN EFFECT OF PARAMETER DESIGN FOR AUTOPILOT TO FLIGHT QUALITY OF AIRCRAFT
    自动驾驶仪的参数设计对飞机飞行品质的影响
    FLYING QUALITY TEST RESEARCH USING BW-1 VARIABLE STABILITY AIRCRAFT
    BW-1变稳飞机飞行品质试验研究
    Time-Domain Maximum Likelihood Method and its Application in the Identification of Aircraft Flying Quality Parameters
    时域极大似然法在某主控飞机等效横航向飞行品质辨识中的应用
    ANALYSIS OF DYNAMIC QUALITY FOR MANEUVERING TARGET TRACKING FIRE CONTROL INTEGRATED SYSTEM
    机动目标跟踪-火控综合系统动态品质分析
    The analysis results indicate that the time-delay feedback may lower down its flutter quality.
    分析结果表明,延迟反馈会降低系统的颤振品质
    Investigation of helicopter mathematical model appropriate for flying quality evaluation
    直升机飞行品质评估数学模型研究
    Tests of the flow quality of the boundary layer wind tunnel at a certain area in Guangxi
    广西某地域边界层风洞流场品质的测试
    Investigation of Visualization Technology for Helicopter Flying Quality Evaluation Process Based on VTK
    基于VTK的直升机飞行品质评估过程可视化技术研究
    The main works of this paper are followed: Analysing the sampled data for measuring steady-state parameters and transient parameters and the quality of AEPSS which are described in MIL-STD-704C and HB6448-90.Developing the software of the system for mearsuring AEPSS by means of software engineering.
    论文的主要工作:根据飞机供电系统性能参数的测试标准MIL—STD—704C和飞机供电系统性能参数的数字式测试方法HB6448-90,系统地研究了飞机供电系统中稳态、瞬态性能参数的特性以及供电品质测试的理论和方法,并且运用软件工程的方法设计飞机供电参数测试系统的软件。
    The main task is to inspect and control AC and DC power bus, EMPC and the quality of external power.
    其主要任务是对主交流、主直流汇流条和机电式功率控制器(EMPC)进行监测和控制,并对外部电源的品质进行监控。
    Based on the primary principle of flight dynamics, the paper studies the flight quality of Tailless Flying-wing HALE UAV and Taill Flying-wing according to traditional calculation methods.
    本论文以经典飞行动力学原理为基础,利用传统的飞行力学计算分析方法,对飞翼布局的高空长航时无人机的飞行品质与有尾飞翼布局和常规布局的飞行品质进行了对比研究。
    The test results converted under standard conditions are given and compared with the relative requirements of the military helicopter flying quality specification HB6105-86. Lastly, the objective and reasonable conclusions have been drawn.
    给出了换算到标准条件下的试验结果,并与军用直升机飞行品质规范HB6105-86的有关要求进行了比较,并得出了结论。
    Based on Linux, software of the helicopter flying quality is built with Tcl/Tk, C/C++, and Gnuplot tools .
    基于Linux,运用Tcl/Tk和C/C++,结合Gnuplot共享工具库,本文开发了直升机飞行品质评估系统。
    It's an important part of the "30cm×30cm MSBS system" and "30cm×30cm low turbulence high quality wind tunnel".
    它是我校研制的“30 cm×30 cm磁悬挂天平装置”及“30 cm×30 cm低速高品质气流风洞装置”的重要组成部分。
    It's also an important part of the "300cm×300cm MSBS system" and "30cm×30cm low turbulence high quality wind tunnel".
    磁悬挂天平导航控制系统是“30cm×30cm磁悬挂天平装置”及“30cm×30cm低速高品质气流风洞装置”的重要组成部分。
 

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