分米波仪表着陆系统虚假下滑道的存在会导致飞机得到错误的导航信息。
The plane will receive false navigating information for the existence of false glide path of instrument landing system on decimeter wave band.
飞机配备了UHF和VHF无线电以及仪表降落系统。
The plane has UHF and VHF radios plus an instrument landing system.
飞机配备了UHF和VHF无线电以及仪表降落系统。
The plane has UHF and VHF radios plus an instrument landing system.
本文针对民用飞机发动机综合仪表测试设备，通过对系统功能及技术指标进行分析，提出了测试设备的设计方案。
In this dissertation, for an integrated instrument for civil aircraft engine test equipment, through the system function indices were analyzed by the test equipment design.
无线电高度表测量的是飞机离地面而不是离海平面的距离，用于自动导航及仪表着陆系统上。
Radio altimeters measure the distance of an aircraft above the ground rather than above sea level, they are used in automatic navigation and Blind-landing systems.
水平仪是飞机综合训练模拟器座舱仪表系统中用于显示飞机飞行姿态的仪表，主要完成俯仰、倾斜等指示功能。
Artificial horizon, an instrument of cockpit meter systems of the ACTE, is mainly used to indicate the flight attitude, such as pitching Angle and tilt Angle etc.
当飞行时飞行员可以操纵的每一个系统或部件都要进行操纵，以确定量产飞机与原型机有着相同的性能；在飞行期间，仪表读数要在正常范围之内。
An operational check of each part or system operated by the crew while in flight to establish that, during flight, instrument readings are within normal range.
模拟了飞机的主要系统：飞行系统、视景系统、仪表系统和音响系统。
Most compositions, such as scene system, flight system, flight's sound and control surface are all simulated.
全静压系统检查仪对飞机上该系统的气密性与仪表指示的准确性有直接影响。
Aero pitot-static pressure system tester has direct effects on the airtightness of the air - borne pitot - static pressure system and the accuracy of meter reading.
测试结果表明，民用飞机发动机综合仪表测试设备在人机界面、测量精度和系统运行的可靠性及实时性方面均达到了预定的设计要求。
The results show that the test equipment in the man-machine interface, precision and reliability and real-time systems in terms of both achieved the intended design requirements.
针对一起由静压孔堵塞造成的空难事故，对飞机全静压系统静压孔堵塞后，座舱仪表显示的空速和马赫数进行了分析，讨论了静压孔堵塞后仪表显示速度和马赫数的特点。
After pitot static vents of total static pressure system are covered, the real airspeed, Mach number and pressure altitude are not displayed from cockpit instrument, and the accident might happen.
针对一起由静压孔堵塞造成的空难事故，对飞机全静压系统静压孔堵塞后，座舱仪表显示的空速和马赫数进行了分析，讨论了静压孔堵塞后仪表显示速度和马赫数的特点。
After pitot static vents of total static pressure system are covered, the real airspeed, Mach number and pressure altitude are not displayed from cockpit instrument, and the accident might happen.
应用推荐