摘要
本文简要介绍了一种新型直升机姿态测量系统软件的设计。叙述了姿态测量系统的构成,测量软件的各项功能及其具体实施方法。该软件已在某重点型号直升机全机静力试验中使用,结果表明这种软件的计算方法和数据精度满足了试验要求,取得了成功。
This paper presents a software design of new helicopter attitude measurement system and describes the constitution of attitude measurement system and the functions and use methed of the measurement software.The software was used in the priority helicopter static test.The test result in- dicates that algorithm and data accuracy of the software meets the lest requirements.
出处
《直升机技术》
2005年第4期20-22,共3页
Helicopter Technique
关键词
直升机
静力试验
软件设计
数据处理
helicopter
static test
software design
data processin
