1) Engineering Material Arresting System
飞机道面拦阻系统
2) aircraft arresting system
飞机拦阻系统
1.
The feasibility that aircraft arresting system adopts nonlinear control is analyzed.
针对飞机拦阻系统采用非线性控制进行了机构实现分析,利用状态反馈线性化及线性系统二次性能指标最优控制设计方法设计了非线性控制规律。
2.
An arresting simulation model of an aircraft arresting system for a certain kind of aircraft which has a deflective engagement of a net barrier is established in this paper (the model is also suitable for normal case).
文章建立了某型飞机拦阻系统基于SIMULINK下的飞机撞偏拦阻仿真模型(也适用于非撞偏状况),进行了飞机撞偏拦阻过程仿真,仿真结果表明,此型飞机拦阻系统对撞偏飞机具有很好的纠偏能力。
3.
This paper presents the control principle and method based on the equivalent throttling action of an aircraft arresting system and also presents the simulation of the arresting process by using this method.
文章主要给出了某型飞机拦阻系统基于当量节流作用的控制原理及方法 ,进行了拦阻过程仿真 ,仿真结果表明 ,采用此控制方法设计的系统能够适应不同撞网状况飞机的拦阻。
3) heavy-duty aircraft arresting system
重型飞机拦阻系统
1.
A mathematics model of heavy-duty aircraft arresting system was established by analyzing the Kinematics, Dynamics and researching on the theoretics of water turbine arrester during the arresting period.
在对飞机拦阻系统拦阻飞机期间运动学、动力学以及水涡轮制动器理论研究的基础上,建立重型飞机拦阻系统的数学模型及基于SIMULINK下仿真模型,真实模拟了拦阻系统拦停飞机的过程。
4) Aircraft arresting
飞机拦阻
1.
The cam, controlling the throttle valve hatch, is the key component of the aircraft arresting system.
飞机拦阻系统是一种机场重要的常务保障设施，它用来对正常降落和因意外原因冲出跑道的飞机实施安全拦阻，以保障人机安全。
2.
Equations of motion of the aircraft arresting process taking the elasticity of the arresting cable into consideration were derived with the assumption that the arresting force was completely provided by the tension of the arresting cable.
在假设拦阻力完全由阻拦索提供的前提下,建立了包含阻拦索线弹性变形的飞机拦阻过程非线性动力学模型。
5) aircraft arrestment
飞机拦阻器
6) arresting system
拦阻系统
1.
In this paper,based on the complex analyses of hydraulic system, kinematics, statics and dynamics of system, mathematical model of the designed aircraft arresting system was built, and using simulation method analyse and study the arresting performances.
针对设计的飞机拦阻系统 ,在对其液压系统及拦阻期间运动学、静力学、动力学分析的基础上 ,建立起飞机拦阻系统的数学模型 ,并以MATLAB为仿真软件 ,用仿真方法对拦阻期间的受控参数如飞机过载、拦阻钢缆的拉力、拦停距离等的变化规律进行了分析研究 ,确切模拟了飞机拦阻系统的工作过程 ,对飞机拦阻系统的拦阻性能作了全面的定量分析 ,对改进和改善我国大多数机场的应急着陆设施有着重要意义。
2.
Based on the static and dynamic analysis of soft-ground arresting system,the mathematical model is built.
通过对飞机道面拦阻系统进行静力学、动力学分析,建立了拦阻系统的力学分析模型。
补充资料：飞机校靶(见飞机武器系统校正)
飞机校靶(见飞机武器系统校正)
aircraft boresighting
feiii iiaoba飞机校靶(airerart boresighting)见飞机武器系统校正。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条