Dynamic simulation of aircraft movement examples!
模拟飞机动态移动的例子！
In order to validate validity of the designed fault diagnosis method, simulation researches are conducted with the major failure of certain kind aircraft autopilots flying-controlled box as the ex.
为验证该方法的准确性，以某型飞机自动驾驶仪飞控盒的几种主要故障为诊断源，仿真研究了所设计的综合故障诊断方法。
The simulation results proved that the system can meet the capability indexes of the aircraft brake system and get higher stability, robustness, safety and brake efficiency.
仿真结果表明，系统能满足飞机刹车系统性能指标，具有较高的稳定性、鲁棒性、安全性，达到较高的刹车效率。
The process of aircraft manufacturing is very complex. A simulation model can help engineers understand the complex process and identify the bottlenecks in the systems.
飞机制造过程通常比较复杂，仿真模型可以帮助工程技术人员理解这一复杂的过程和找出系统中的瓶颈。
Simulation of a remote control system of unmanned aircraft with network distributed computing and three dimensional dynamic display and man in loop real time operation is studied.
研究了一种采用网络分布计算，具有三维动态显示、实时操纵和人机闭环的无人机虚拟遥控仿真系统。
System simulation indicates that the electrical power distribute system used in automatic management of aircraft electric load has high reliability and good maintenance.
系统模拟实验结果表明，采用电气负载自动管理技术大大提高了飞机配电系统的可靠性和可维护性。
Characteristic curves of simulation show that whole simulation model and using fuzzy control are comparative with reason; brake performance of aircraft is all right.
仿真特性曲线表明：建立的整体模型和应用模糊控制比较合理，飞机的刹车性能良好。
This paper systematically introduces the ground physical, simulation, of the terrain-following system of the Chang Kong pilotless aircraft designed with the theory of adaptive Angle.
本文系统介绍了用适应角法理论设计的长空无人驾驶飞机地形跟随系统的地面物理仿真。
A boundary element model is established, making use of the ANSYS. In the noise simulation SYSNOISE is applied to get estimable simulation results of aircraft noise close to ground.
建立了某型军用飞机的ANSYS边界元模型，用声学有限元-边界元仿真软件SYSNOISE进行了噪声仿真，获得了飞机噪声在地面附近的辐射结果。
In aircraft designing process based on modeling and simulation, there exists a vast amount of uncertainty, which causes modeling predictions to differ from reality.
在基于建模和仿真的飞行器设计过程中，由于客观存在的不确定性，导致了模型预测结果与真实情况的不一致。
The simulation results indicated that this sequencing method could reduce the total delay of the system as much as possible, by setting the weights for main factors which affect aircraft sequencing.
仿真结果表明，模糊综合评判排序方法通过设置各因素权重，可在综合考虑各因素的基础上使得系统总延迟尽量减少。
This paper introduces the software structure and model libraries design of a distributed comprehensive simulation platform for the mechanical and electrical systems on aircraft.
该文介绍了分布式机载机电设备综合仿真平台的软件结构和模型库设计及仿真实例运行过程。
The three dimension module of aircraft, terrain and object are erected, and real time three dimension visual simulation of is 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 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。
According to mathematical model of load force, the paper has designed a simulation system of aircraft force-feeling system by the method of electro-motive force servo loading.
依据飞机纵向操纵负载力的数学模型，采用电动式力伺服加载的方式设计了飞机纵向操纵人感仿真系统。
The finite-element simulation models of the discrete rod and the projectile impacting on the aircraft panel structure at high velocity are established according to some experiment projects.
根据已有实验方案分别建立了离散杆和射弹高速冲击飞机壁板结构的有限元模型，利用显式动力有限元计算程序进行了冲击损伤仿真。
On the basis of the vehicle oriented parameters and the aerodynamic characteristics, the history of takeoff is emulated. Simulation studies show that the model is useful in the aircraft design.
该模型包含了起落架系统特性和全机气动力特性，根据飞机总体设计参数可仿真给出其起飞性能指标。
Simulation based on test data to analyze thedynamic characteristics of the model, research aircraft stopping distance, overload and cableforce relationship in the parameters.
基于仿真试验数据，对模型的动态特性进行分析，研究拦阻过程中飞机的拦停距离、过载、拦阻索拉力等相关参数之间的内在联系；
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。
Taking the lateral flight control system of an aircraft as an example, simulation was carried out for the cases with perturbing parameter and interference.
以某型飞机侧向飞行控制系统为例，针对系统参数摄动和承受有界干扰情况，对所提出的方法进行了仿真分析与验证。
The developing procedures and technical problems in developing virtual cockpit can be helpful to the simulation and development of other civil aircraft cockpit system.
本论文涉及到虚拟座舱的开发流程和开发中的一些技术问题，因此对其它民用飞机座舱系统的仿真开发具有一定的借鉴意义。
The design and simulation of the yaw pointing mode dynamic decoupling fuzzy control system for an aircraft are studied in this paper.
用该综合方法对某型飞机的侧向直接力控制模态(航向指向)进行了分析与设计，并将其与动态逆方法进行了比较。
The present system of the most important part of the aircraft cabin is the manipulation of the body electric load, which can be requested by a variety of sensory manipulation of the simulation.
本系统实现的最重要部分是对飞机座舱操纵机构的电动加载，通过它可以实现所要求的各种操纵感觉的模拟。
The results of the simulation may provide a theoretical basis for the design of height lift devices of large aircraft in ground effect.
该文研究结果可以为大型飞机的增升装置地面效应设计提供参考依据。
Simulation result indicates that the equivalent moment derivatives model can be used in the evaluation of aircraft conceptual design and flight control system design.
验证表明，等效力矩导数模型可用于评估设计方案或指导飞行控制系统设计。
Simulation result indicates that the equivalent moment derivatives model can be used in the evaluation of aircraft conceptual design and flight control system design.
验证表明，等效力矩导数模型可用于评估设计方案或指导飞行控制系统设计。
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