The flight scene simulation is an important part of the flight simulation, and its visual effect and reality degree will influence the whole flight simulator directly.
飞行视景仿真是飞行仿真的一个重要组成部分，它的视觉效果和逼真程度将直接影响整个飞行模拟器的逼真度。
Visual flight simulation system combines three-dimensional computer graphics animation with flight numerical simulation for depicting flight process of Unmanned Air Vehicle (UAV) on computer screen.
飞行可视化仿真系统采用计算机三维图形动画与飞行数值仿真相结合的设计方法，在计算机屏幕上再现无人机的飞行过程。
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 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。
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。
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。
Su-27 flight simulation system is a full mission simulation system which is directed at the third generation of military aircraft and applies the modern advanced technologies.
“苏二七飞机飞行仿真系统”是一个典型的针对第三代军机、运用现代先进技术研制成功的全任务仿真系统。
In accordance with flight simulator's demand of motion simulation system motion performance, the electro-control part of flight simulation test prototype is reconstructed in this paper.
本文依据飞行模拟器对其运动模拟系统运动性能的要求，对飞行模拟试验样机电控部分进行了改造。
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。
The fly-by-light system is demonstrated with a prototype based on fibre channel protocol which has been applied to communications between flight control system and flight simulation system.
该系统通过实现了一个基于光纤通道协议的原型系统得到验证，已成功应用于飞行控制系统与飞行仿真系统之间的通信。
Through construction of a distributed flight simulation system based on RT-LAB platform, the outer characteristics of the navigation system were achieved with hardware-in-the-loop simulation.
利用RT -LAB平台构建分布式飞行仿真系统，实现导航外部特性的半实物仿真。
In this paper four model following approaches are used to design Hydraulic Velocity Flight Simulation Table with One Axis.
本文讨论了将模型跟踪综合技术用于单轴液压速度转台综合设计的四种方法。
In this paper four model following approaches are used to design Hydraulic Velocity Flight Simulation Table with One Axis.
本文讨论了将模型跟踪综合技术用于单轴液压速度转台综合设计的四种方法。
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