The reel functions are hydraulically powered and controlled from the unit control cabin.
从控制室可液压带动和控制卷筒。
The experiment was carried out by using a computer system, aHead-up Display (HUD) system, and the analog control cabin of Fighter-5.
本实验是通过计算机系统、平视显示器系统及歼- 5模拟驾驶舱实现的。
The last but not the least, the electrical wiring of vector inverter control cabin and design of computer control and data acquisition system are introduced.
最后简单介绍了本课题矢量控制变频控制柜的外部附件电气接线、计算机控制及数据采集系统的硬件设计等内容。
Firstly, the situation of excessive dynamic stress during vibration test of environmental stress screening for an air-air missile flight control cabin was introduced.
首先介绍空空导弹飞控舱环境应力筛选随机振动试验过程中出现振动过应力的情况，然后对出现振动过应力的原因进行了分析。
This automatic test equipment can automatically diagnose and test the nose cabin and control cabin of a missile and training missile, and it enhances the test efficiency and reliability.
该系统可对导弹前舱、控制舱及训练弹进行自动诊断测试，能提高导弹检测的效率及可靠性。
Communication system is an important part of improved aerial defence system, and the key of the project is realizing high speed and real time communication between control cabin and equipment cabin.
进行升级改造后，通信系统是各装备之间协同工作的关键所在，该项目的关键就是在设备舱与操作舱之间实现高速的准实时通信。
As well as being able to control features of the aircraft seat, such as cabin crew alerts and volume controls, services such as destination content and information about activities are also included.
这一功能除了可以控制如乘务员呼叫和音量控制等座位上的服务以外，还增加了目的地和活动的信息。
Cabin crew will control the movement of seats, most likely with a tablet or smart phone, while passengers would need to inform airlines of their height at check-in.
座位的移动将由机组人员控制，很可能是通过平板电脑或手机操作，旅客只需在值机时将自己的身高告知航班人员即可。
The pressure control systems provide cabin differential pressure by controlling the outflow of air from the faselage.
压力控制系统通过控制机外气流来提供客舱压力差。
The new concepts of virtual cabin, virtual central control room, virtual bridge and virtual control panel are presented and discussed.
提出虚拟机舱，虚拟集控室，虚拟驾驶台，虚拟控制仪表板的新概念并讨论其可实现性。
Shown here is the control panel inside the cabin, photographed during the second stage of her row.
这里展示的是机舱内的控制面板，在她连续第二阶段的拍摄。
This paper shows by means of the analysis of controllability and observability that the present cabin pressure control system is not controllable for all. states, so it is not a good method.
本文通过可控性分析和可观察性分析指出，现有的舱压控制系统不是状态完全可控制的，因而不是好的方法。
This paper shows by means of the analysis for controllability and observability that the present cabin pressure control system is not controllable for all states, so it is not a good method.
本文通过可控性分析和可观察性分析指出，现有的座舱压力控制系统不是状态完全可控制的，因而不是好的方法。
In order to realize the close-loop control to the cabin, three target points on the cabin must be got to solve the position and orientation of the cabin.
为了实现对馈源舱的高精度控制，需要精确测量馈源舱上不共线的三个目标点的坐标，实时确定馈源舱的位置和姿态。
This paper presents the analogized methods and the active control experiments of the cabin noise for a propeller airplane.
本文介绍螺桨飞机舱内噪声的地面模拟方法和主动控制实验。
Cabin pressure regulation system experimental platform distributed control system is designed based on expert PID control principles.
座舱压力调节系统试验台集散控制系统根据专家PID控制原理设计。
Considering the unique cabin environment, a new cabin air quality control system based on active and passive control strategy was described.
针对旅客机独特的座舱环境，提出一种新型的主动与被动控制策略相结合的座舱空气质量控制系统。
This paper introduces the characteristics of the cabin atmosphere of AIP submarines, presents the particularities and key technologies that applied in the cabin atmosphere control system.
介绍了AIP潜艇舱室大气环境特点和系统控制的特殊性以及系统控制的关键技术，并为aip潜艇舱室大气环境控制系统的设计提供参考。
It mainly is used to assure the temperature on the ship so that control the cabin temperature. Your best choice.
主要应用于航海领域确定温度，对于控制船舱内部温度是一款不错的选择材料。
The temperature control of the aft cargo compartments is similar to that of the cockpit and cabin temperature-control system in the heating mode.
后货舱与驾驶舱和客舱的温度控制系统在加热模式下相似。
So an active noise cancellation (anc) system for helicopter cabin noise based on adaptive internal model control technique, is developed in laboratory.
从而在实验室构造了一套基于自适应内模控制技术的主动消声系统(anc)。
Based on the nonlinear and time varying parameter of the cabin pressure regulating system characteristics, a control strategy of fuzzy sliding mode variable structure control is proposed.
针对座舱压力调节系统的非线性和参数时变特性，提出了模糊滑模变结构控制方法。
In this paper the active noise control in cabin is discussed, and some successful examples are presented, such as active noise control in cabin of aircraft and of autocar.
首先讨论了有界空间的有源噪声控制，并给出了一些较为成功的舱室有源噪声控制实例。例如，飞机座舱内和小汽车座舱内有源噪声控制系统和它们的降噪效果。
Automatic temperature control unserviceable, cabin temperature goes below 10 degrees (falls below plus 7 degrees).
自动温度控制失效，舱内温度降到10度(下降到正七度)。
Objective To research and evaluate the ventilation and heat exchange character of the sealed-cabin temperature and humidity control system in manned space flight on the ground.
目的在地面条件下研究、评估载人航天飞行中密闭舱内温湿度控制系统的通风和换热特性。
Based on the nonlinear static equivalent equations of the cable-cabin system, forces and lengths suitable for servo motor control are obtained by least square method and an optimum strategy.
基于系统的非线性静平衡方程 ，通过最小二乘运算和优化策略 ，获得了适于伺服电机控制的索系平衡张力和索长。
Based on the known refrigerating output, the thermoregulation of the operator cabin is realized through adapting PID control strategy controlling the rotating speed of the evaporator fan.
在确定的制冷量基础上，采用PID控制策略来控制蒸发器风扇的转速，从而实现驾驶室内的温度调节。
Based on the known refrigerating output, the thermoregulation of the operator cabin is realized through adapting PID control strategy controlling the rotating speed of the evaporator fan.
在确定的制冷量基础上，采用PID控制策略来控制蒸发器风扇的转速，从而实现驾驶室内的温度调节。
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