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。
By using the method, it can effectively analyse the aerocraft Simulate Training System's failure.
在搭建的一类C3I系统平台上，研究了系统的飞行器模拟器节点的特点及其功能。
The characteristics and functions of aerocraft simulator are studied based on a structured generic C3I system test-bed.
在某飞行器模拟加载系统中，使用此方法进行转动惯量的测量和多余力的消除，取得了较为理想的结果，对电动加载系统的进一步研究具有参考价值。
The elimination of plus torque in electric loading system is resolved well by this method, and it has referenced value to thorough research in electric l...
SharonChrista McAuliffe受邀对美国宇航局的KC-135型模拟“零重力”飞行器进行测试。
Sharon Christa McAuliffe received a preview of microgravity during a special flight aboard NASA's KC-135 "zero gravity" aircraft.
高超声速飞行器的设计工具，即地面试验、计算和飞行试验，在模拟高超声速飞行方面都有其局限性。
The developing tools for hypersonic vehicle, i. e. ground test, computation and flight lest all have limitations for simulating hypersonic flight.
它是地面半实物仿真系统中的一种重要专用设备，用来模拟飞行器舵机在飞行过程中所承受空气动力力矩载荷。
It is an important half hardware-in-loop simulation equipment, which is often used to simulate the aerodynamic torque load on the missile rudder or elevon actuators in the flight.
配橡胶内衬的复合材料板壳可以模拟宇航飞行器的纤维缠绕压力容器。
Composite plate and shell with rubber liner can simulate filament wound pressure vessels of the aircraft.
摇摆台作为一种空间运动机械被广泛用来模拟舰船、车辆、飞行器、陀螺仪的运动姿态等。
Swaying test platform, as a space motion mechanical device, can simulate motion of ship, vehicle, space craft, gyro and so on.
介绍了超音速飞行器的气动光学效应，并讨论用数值模拟来研究和预测气动光学效应的方法。
The aero - optic effect of supersonic vehicle is introduced in the paper. The methods used for studying and predicating the aero - optic effect with numerical simulation is discussed.
对航天飞行器防热部件在氧煤油发动机火焰喷吹下的烧蚀行为进行了有限元数值模拟。
The ablation behavior of spacecraft thermo-resistance components under blowing by oxygen-kerosene flame is investigated by means of finite element numerical simulation.
轨道计算主要用来模拟飞行器的飞行过程，前提是建立动力学模型。
The main function of orbit calculation is to simulate the flight procedure of spacecraft, before that, the dynamics model of orbit must be established.
虚拟仪表是模拟飞行器或汽车的虚拟场景中必不可少的元素，为虚拟场景提供了良好的人机交互界面。
Virtual instruments are important elements in a virtual scene which contain virtual flying objects or automobiles to provide interactive interface between operators and the scene.
当它不是在这份报告范围内时，为提供一设计飞行草图，描述了一个象征性的，圆锥形的飞行器来提供垫托物作为讨论和飞行模拟。
While it is not within the scope of this report to provide an engineered flyer design, a notional, cone-shaped flyer is described to provide a substrate for the discussion and flight simulations.
电弧等离子体风洞是一种能产生高温、高压的热源设备，用于在地面模拟航天用再入式飞行器的气动环境。
Plasma wind tunnel is equipment which can generate high-temperature and high-pressure to simulate the air environment of aerospace reentry vehicles.
惯导测试转台作为航空航天领域中进行模拟、仿真、测试的关键设备，在飞行器的研制过程中起到重要作用。
In the aviation and aerospace research field, inertia test and motion simulation table plays important roles in the research and development of inertial devices and aviation arrangements.
模拟月球表面极端高低温环境，对空间飞行器机构活动部件常用固体自润滑材料进行极端温度环境存贮实验。
The extreme temperature adaptability of solid lubricant used in space components was investigated by simulating the temperature environments on the moon surface.
对飞行器及其部件进行气动力数值模拟时，气动外形常常是以离散数据形式给出。
When aerodynamic numerical simulation for flight vehicle and its components is conducted, the aerodynamic shape is generally given in the manner of discrete data.
建立了飞行器、地形、地物的三维模型，利用计算出来的数据进行飞行器的实时三维视景仿真模拟。
The three dimension module of aircraft, terrain and object were erected, and real time three dimension visual simulation of was executed through computed data.
建立了飞行器、地形、地物的三维模型，利用计算出来的数据进行飞行器的实时三维视景仿真模拟。
The three dimension module of aircraft, terrain and object are erected, and real time three dimension visual simulation of is executed through computed data.
介绍了线阵CCD遥感器单轴转台的工作原理，分析了转台模拟飞行器成像的误差，给出了转台的指标及参数设计。
This paper introduces working principle of liner CCD remote sensor uniaxial turntable, analyses imaging error of turntable simulation flying and brings point and parameter design of turntable.
文中在物面无滑移边界条件的基础上施加物面绕体轴的切向速度，通过求解定常ns方程对飞行器滚转进行模拟。
In the paper, the steady NS equation was solved to simulate aircraft roll by adding tangent velocity to no slip wall boundary condition.
结果表明，CARIA校准箱是先进的飞行器动力模拟器校准设备，可以满足对动力模拟器推力和质量流量的精确校准。
It can be seen that calibration tank in (CARIA) is a set of advanced facility for calibration of aircraft engine powered simulator and it can be used to calibrate simulators accurately.
为了研究微型飞行器的飞行机理以及节约风洞实验资金，进行了微型飞行器的数值模拟方法研究。
To study the flying principle of micro-air vehicle (MAV), and to economize the test outlay of wind tunnel, the numerical simulation of MAV is introduced in this paper.
应用数值方法模拟了飞行器升力面下表面喷气的增升作用。
The aerodynamic characteristics of an airfoil with a jet issuing from its lower surface are investigated by numerical method.
本文提出了一种可模拟飞行器翼面等溥壁结构的强刚度可靠性分析方法。
In this paper, a method of strength and stiffness reliability analysis for bar plate structural systems, which can simulate the wing of the flyers, is presented.
实验系统不但能够模拟柔性航天结构的运行环境，还能对由于航天飞行器的机动和折叠结构的展开而引起的振动进行模拟。
This system could emulate not only the work conditions, but also the motion of space structures and deployment of the foldable structures.
通过建立扇翼飞行器的二维数学模型进行模拟分析、设计试验模型并进行了相关实验比较分析，证明垂直升降的可行性。
According to comparative analysis between the 2d mathematical model simulation and the of test model design of fan wing aircraft, the feasibility of VTOL is proven.
对一种轴对称形式的高超声速飞行器全流道开展了风洞实验和数值模拟研究，分析了不同来流总压、飞行攻角全流道的流场结构和气动力特性。
This paper presents a numerical simulation of separated flow over an airfoil at large attack angles with oscillating excitations to study separation flow control over an airfoil.
对一种轴对称形式的高超声速飞行器全流道开展了风洞实验和数值模拟研究，分析了不同来流总压、飞行攻角全流道的流场结构和气动力特性。
This paper presents a numerical simulation of separated flow over an airfoil at large attack angles with oscillating excitations to study separation flow control over an airfoil.
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