Earlier this year, InterSense's IS-900 system was successfully integrated into the F-35 engineering simulators to test all components and procedures related to the aircraft.
今年的早些时候，IS- 900系统已经被成功的集成到F - 35工程学模拟器中，用来测试与该飞机相关的所有部件和程序。
The CATbird is a modified 737 designed to test, integrate, and validate the full F-35 mission systems suite in an airborne environment before the system flies in an F-35 aircraft.
该测试台是波音737改进型，旨在飞行前对机载环境下f - 35任务系统套件进行测试、集成和验证。
It can be used in the flight test of aircraft performance, controllability, stability, and aircraft system, as well as the flight path measurement of some guided weapons.
该系统可用于飞机性能、操稳和系统试飞的测试，也可推广用于某些制导武器的弹道测试。
This paper introduces the structural filter design of a variable stability aircraft control system and the ground test of structural resonance.
本文介绍变稳飞机控制系统结构滤波器设计及结构谐振地面试验。
Presently the performance test of the Aircraft power Supply System still relies on manual methods, which cause a waste of manpower, material resources and time.
目前飞机电源系统的性能检测主要还是采用人工测试的方法，往往需要耗费大量的人力、物力和时间。
To meet the needs of certain type of aircraft avionic system ground test, a set of air data computer stimulating system was designed.
针对某型飞机航电系统地面试验的需要，设计了一套大气数据计算机激励器系统。
The energization of the aircraft electrical circuits starts a full test of the ventilation system. The test continues for 2 minutes approximately.
给飞机电路通电，将起动通风系统全测试。该测试将持续大约2分钟。
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.
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。
Through ground test, suitable parameters of the structural filter are selected and the coupling between the flight control system and the aircraft elasticity structure is effectively restrained.
通过试验，选择了合适的结构滤波器参数，有效地抑制了飞行控制系统与飞机弹性结构之间的耦合。
To realize numeralization, automation and flexibility during large aircraft components assembly, a novel posture alignment and joining test system for large aircraft fuselages is developed.
为实现飞机大部件装配过程的数字化、自动化和柔性化，研制了大型飞机机身调姿与对接试验系统。
A Robust design approach and integrated test procedure of the aircraft variable geometry inlet control system are discussed.
论述了飞机进气道可变几何形状控制系统的鲁棒设计方法和系统的综合试验。
Helicopter flight load test of rotor system dynamic components is the key part of flight load test of the whole aircraft, and is also the basis of helicopter life reliability calculations.
直升机旋翼系统动部件飞行载荷测量是全机飞行载荷测量的关键，也是直升机寿命可靠性工作的基础。
The central control component or the controller is the core and heart of an aircraft, and the test system we developed is used to test and verify the controller.
控制分组件是某飞行器的核心部件，而控制分组件测试系统是为控制分组件研制测试设备。
Work will also continue on the other five flight test aircraft and the subsequent aircraft in the production system.
另外五架试飞飞机以及其它正在生产中的飞机的相关工作也在进行中。
The system can automatic test and fault diagnosis to self-propelled anti-aircraft gun weapon system. The model obtain a good result through a series of experiments, it provide a ap...
通过实验对系统进行了实例应用和验证，取得了较好的效果，为自行高炮武器系统的技术保障提供了一种实用的方法。
The system can automatic test and fault diagnosis to self-propelled anti-aircraft gun weapon system. The model obtain a good result through a series of experiments, it provide a ap...
通过实验对系统进行了实例应用和验证，取得了较好的效果，为自行高炮武器系统的技术保障提供了一种实用的方法。
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