He recently demonstrated a computer simulation of the idea to researchers at the Goddard space Flight Centre, one of the main scientific establishments of NASA, America's space agency.
他最近在美国国家航空NASA的主要科学机构之一，Goddard太空飞行中心(GoddardSpace Flight Centre)用电脑模拟向研究人员示范了设计的可行性。
The team used simulation tools to show it was possible to achieve over-land flight by dramatically lowering the level of sonic booms through the use of an "inverted-V" engine-under wing configuration.
这个团队在其所设计的飞机模型中在引擎上方使用了一个“倒V字型”的结构，他们通过模拟工具展示了通过这个结构可戏剧性地减少音爆导致的噪声成为一种可能。
Alenia Aeronautica is developing a C-27J Spartan full flight simulator for the Italian Air Force using Concurrent's multi-processing system as the simulation host system.
阿莱尼亚航空公司正在为意大利空军开发c - 27j斯巴达全面飞行模拟器，利用Concurrent的多处理系统作为模拟主机系统。
On the basis of output of flight imitate system, the driving signal of flight simulation is formed by coordinates transforming, scale limiting, signal washout and filter.
根据飞行仿真模块的输出，通过坐标变换、比例限制、信号洗出和滤波等，形成运动平台的驱动信号。
Fidelity Technologies Corp. will provide classroom and simulation training for naval aviators and flight officers under a new five-year, ＄68 million contract with the NAVAIR Training Systems Division.
根据一份美国海军航空兵武器系统部训练系统分部新授予的为期五年，总价值6800万美元的合同，Fidelity技术公司将为海军飞行员和飞行官员提供教室仿真训练。
The GEOS-5 model runs on the Discover supercomputer in the new NASA Center for Climate Simulation at Goddard Space Flight Center. Discover contains nearly 15,000 processors and will soon be augmented.
GEOS - 5模型在戈达德太空飞行中心新建的美国国家航空航天局气候模拟中心的“探索”超级计算机上运行，它拥有约15000个处理器，并且即将增加。
The GEOS-5 model runs on the nearly 15,000 processors of the Discover supercomputer in the new NASA Center for Climate Simulation at Goddard Space Flight Center.
在NASA戈达德宇航中心新建的气候模拟中心的超级电脑“探索”上有将近15000个处理软件在运行GEOS - 5。
The GEOS-5 model runs on the nearly 15, 000 processors of the Discover supercomputer in the new NASA Center for Climate Simulation at Goddard Space Flight Center.
在NASA戈达德宇航中心新建的气候模拟中心的超级电脑“探索”上有将近15000个处理软件在运行GEOS - 5。
These are just highlights but, IMO, this is the most advanced flight model yet for a PC Simulation title.
以上只是一个概要，在我看来，这是迄今PC机模拟方面的最先进飞行模型。
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.
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。
Objective To study the optimized method for precise modeling of virtual device, while using virtual reality in the simulation training of space flight.
研究在应用虚拟现实进行航天飞行模拟训练时，虚拟设备精确建模的实现与优化方法。
The system can give user plentiful and visually result of simulation; consequently help them accomplish the design, validation, argumentation, filter and decision of flight scheme.
系统为用户提供大量的、可视化的仿真结果，从而协助他们完成飞行方案的设计、验证、论证、筛选和确定。
It first discribes discribes the fonction and component of synthesis simulation system, then it gives the design idea and frame of operation flight program.
首先对综合仿真系统的功能和组成作了简要介绍，然后给出了作战飞行软件的设计思想和框图。
Finally, full envelope simulation results from different flight conditions show that the guidance law can meet the requirement of both precision and angular constraint of airborne dispenser.
在不同飞行条件下的全弹道仿真结果表明，该导引律均能同时满足布撒器在抛撒点精度和期望姿态角要求。
Through a large number of computer digital simulation experiments, this paper discusses the shift time of free flight and little single impulse individually.
本文通过大量的计算机数字仿真实验，研究了无冲量自由飞行轨迹与单个小冲量飞行轨迹的转移时间。
On the reasonable assumption of match AOA (Angle of attack) flight, the mathematics simulation model of the reentry flight of a spaceship is formulated in this paper.
在配平迎角飞行的合理假设下，建立了描述载人飞船再入飞行段弹道的数学仿真模型。
In this paper, the function and role of the keyboard simulation system for Flight Simulator are explained.
阐述了飞行模拟器仪表仿真系统的功能、作用。
Simulation of SSR blips, flight turns, flight level changes, speed adjustments, initialization or dynamic deployment of airplane position and status within authorization.
模拟二次雷达信号功能、实现飞机的转弯、高度上升下降、速度调配，在授权范围内，初始化或动态调整飞机位置及状态。
In the paper, the application of feedback linearization in the flight control is described firstly, then the simulation demo system of nonlinear flight control system is designed.
文中首先采用反馈线性化理论设计了非线性飞控系统，进一步设计了非线性飞控系统仿真视景演示平台。
This paper describes the classification of the flight simulation technology, including mathematical simulation, hardware in loop simulation and man in loop simulation.
叙述了飞行仿真技术的分类，包括数学仿真、含实物仿真和人在回路中的仿真。
This paper first studies the pointing error, rate stability error, and amplitude phase error of the flight simulation turntable, then gives out specific calculation method for pointing error.
对三轴飞行模拟转台的指向误差、速率稳定度误差及幅相误差进行了研究，对其指向误差给出了具体算法，并针对一种转台的具体精度指标而算出了各项误差。
The flight benchmark status is defined according to the basic requirements of flight simulation, and the equations are solved by the numerical methods.
根据飞行模拟的基本要求，定义了飞行基准状态，并采用数值计算的方法对方程求解。
It is widely used in the fields of flight simulation, flight controller design, and so on.
本系统可广泛应用于飞行模拟、飞控器设计等领域。
Originally developed by Stanford University and NASA, force-feedback technology was first used for flight simulation.
强力反馈技术最初由斯坦福大学和美国国家航空航天局开发，起初仅用于飞行模拟。
The near deadbeat control design was applied to an aeroengine speed simulation system for flight handling simulation.
本文研究了飞行训练用航空发动机转速模拟系统拟最少拍控制设计。
The design and realization technology suitable for integrated real-time simulation device of UAV flight control are presented. The practice and application is emphasized.
本文给出了适于无人机飞行控制的集成化实时仿真设备的设计与实现技术，着眼于工程实践和应用。
This project is not only an improvement to the architecture but also an expansion of system's function, which means a lot to the missile flight simulation and the final navigation system.
该项目的完成不仅使惯性元件测评系统在结构设计上有了较大改进，在功能上也使其更加完备，向着最终的弹体飞行仿真及导航系统的实现迈出了一大步。
As the system's "software bus", CORBA connects the stage of flight simulation modeling environment and the long-distance model warehouse and algorithms library.
CORBA作为系统的“软总线”把飞行仿真建模环境的前台和远程的模型库和算法库连接起来。
Finally, a complete set of UAV flight visual simulation is obtained, which lays the foundation of designing and simulating of UAV for the future research.
最终得到了一套完整的无人机可视化仿真系统，从而为今后的无人机飞控器设计与飞行模拟研究奠定了基础。
Finally, a complete set of UAV flight visual simulation is obtained, which lays the foundation of designing and simulating of UAV for the future research.
最终得到了一套完整的无人机可视化仿真系统，从而为今后的无人机飞控器设计与飞行模拟研究奠定了基础。
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