flight test system的例句大全

On multiple channel automatic control system, implementing the flight-flight test profile in random sequence

在多通道自动协调加载系统上实现飞行顺序随机的飞-续-飞试验载荷谱

Design of a Combined Intelligent Test Equipment for Flight Parameter Recording System

飞行参数记录系统综合智能检测设备的设计

A kind of new flutter analysis method ( robust flutter margin method) were introduced. Pass to incorporate organically the flight test data and the system model, make use of the structured singular value theories proceed the flutter boundary estimate.

一种新的颤振分析方法&鲁棒颤振裕度法被介绍，它利用结构奇异值理论将系统模型和试飞数据有机结合起来进行颤振边界预测。

A Flight Test Method Research on Instrument Landing System Applied to a Far Zone

仪表着陆系统远区场飞行检验方法研究

By choosing particular course and data processing, this method is suitable for flying test on the far zone of instrument landing system, and can be used for making a statistical analysis to the flight test result.

从理论上分析表明，通过选择特殊的检验航线及数据处理方式，此方法可适合于对仪表着陆系统远区场进行检验，且可对检验结果进行统计分析。

Airborne Testing System Based on Network and its Application in Flight Test

基于网络的试飞机载测试系统及其应用

Oracle Database Backup and Recovery in Flight Test and Measurement Engineering Database System

飞行试验数据库系统中Oracle数据库的备份和恢复

As the main transportation facility of the flight area field road system, the mechanics performance or health status of the taxiway bridge is related directly to the airport safety. So, it is necessary to test its health and assess its mechanics performance regularly.

滑行道桥作为飞行区场道系统内主要的交通设施，其力学性能或健康状况直接关系到机场的安全运营，因此，必须定期对滑行道桥结构进行健康测试与力学性能评定。

The flight test monitor and command system is main part of flight test engineering.

试飞监控与指挥系统是飞行试验工程中的重要组成部分。

Building and Application of Flight Test Monitor and Command System

试飞监控与指挥系统的建立及应用

Digital attitude control system and flight test results of Chinese RETURNABLE SATELLITE

返回式卫星数字姿态控制系统及飞行试验结果

The illogicality that current accuracy evaluation method for missile weapon system is analyzed. Based on synthesizing simulation information and flight test data, a new idea is presented by using Bayes small sample statistical theory, which evaluates accuracy of missile weapon system.

在对现行导弹武器系统制导精度鉴定方法的不合理性分析的基础上，提出了综合数学仿真模拟打靶验前信息并结合Bayes小子样统计理论来进行导弹武器系统制导精度综合鉴定的新思路。

Study on Control System Failure Mode during Air Defense Missile Flight Test

防空导弹飞行试验控制系统故障模式研究

Distributed Virtual Flight-test System simulates the missile strike process, which facilitates the development of a new generation of weapon systems, the research of this simulation system can effectively save the military outlay, shorten the development cycle and improve efficiency.

分布式虚拟靶试系统是为了方便新一代武器系统研制而建立的用于模拟导弹打靶过程的仿真系统，该系统的开发可以有效地节省经费，缩短研制周期，提高研制效率。

Finally, concludes the results of open system test, flight experiment and imaging of moving targets with the prototype system.

最后，总结了在原理样机基础上的开放实验、飞行试验和运动目标检测实验。

flight test analysis of an improved transfer alignment for missile strapdown inertial guidance system

弹载捷联惯性制导系统传递对准技术试飞验证

high lift system design for a supercritical wing flight test plane

超临界机翼飞行验证机的增升装置设计

based on the object-oriented programming method, an integrated simulation system software is developed to simulate the whole real-time flight liquid height, and to provide a perfect software environment for the development, debug, digital algorithm test and performance evaluation of the on-board software.

基于面向对象技术，用类的程序设计方法，开发出通用的实时仿真软件系统平台，用于实现火箭飞行液位系统数字仿真，为系统的开发、调试和数字算法及性能评估提供软件环境。

How to advance the test speed of air data ( UAV) is an important item in improvement of flight control system performance.

无人机大气数据（高度、空速）的检测速度关系到飞行控制系统的性能。

the research object of the dissertation is to design, assemble and debug the equipment, which could realize the system performance test and fault allocation detection for fcc-86e flight control computer.

本文研究目的是研制FCC-86E飞控计算机的检测设备，该设备能对FCC-86E进行系统性能测试和故障定位。