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。
Computer temperature control simulation shows that this arithmetic has obtained satisfactory control effect in instant heating system for aircraft deicing vehicle.
针对飞机除冰车快速加热系统的计算机温度控制仿真结果表明获得了令人满意的控制效果。
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。
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。
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。
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。
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。
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。
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。
In order to quantitatively analyze the flight risk for wing icing, the probability assessment was proposed in which the simulation data of the pilot-aircraft-environment system was utilized.
考虑结冰对临界迎角、升阻特性等的影响，通过建立非线性动力学仿真模型和特殊情况下驾驶员操纵副翼偏转模型，实现了机翼结冰后的人-机系统动态仿真。
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 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。
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