带动力模型自由飞试验测试系统设计与实现  

Design and Implementation of Test System for Trop Model Test With An Engine

作　　者：安玉娇[1] 江辉军 郑浩[1] 

机构地区：[1]中国飞行试验研究院飞机所,陕西西安710089 [2]中航工业第一飞机设计研究院飞控液压所,陕西西安710089

出　　处：《测控技术》2015年第6期132-135,共4页Measurement & Control Technology

摘　　要：分析了带动力模型自由飞试验测试系统设计要求及关键点,介绍了测试系统传感器的选型和基于片上系统的采集器设计方法,阐述了测试系统原理及软硬件实现,并以地面试验数据为例进行了数据的预处理和分析。试验验证表明,设计的测试系统满足了试验的测试要求,对同类测试系统具有参考价值。Design requirements and the key points of testing system for a certain trop model test with an engine are analyzed, the selection of sensors and the design method of collector based on system on chip are intro- duced, the principle and the implementation of software and hardware of the test system are elaborated. The ground test data is taken as an example for data preprocessing and analysis. The test proves that the designed test system meets the test requirements, and provides a certain reference for the similar test system.

关 键 词：模型自由飞 测试系统 飞行试验 片上系统 

分 类 号：TP311.52[自动化与计算机技术—计算机软件与理论]