摘要
本文对用于飞行器极性测试的六自由度并联台进行了研究,分析了六自由度并联台技术背景及其在飞行器极性测试领域应用的可行性,给出了六自由度并联台总体设计方案,对平台关键指标进行了仿真验证,系统地阐述了六自由度并联台在飞行器极性测试应用过程中的关键技术和方法。
This paper studies the six-degree-of-freedom parallel platform used for the aircraft polarity test while analyzing the technical background of the sextuple redundancy parallel platform and its application feasibility in the field of aircraft polarity test.With the general design scheme of six-degree-of-freedom parallel platform introduced and the simulating verification of platform key indicators conducted,the key technologies and methods for the application of six-degree-of-freedom parallel platform in aircraft polarity test are elaborated systematically.
作者
鞠新星
胜永民
李明章
高祥
Ju Xinxing;Sheng Yongmin;Li Mingzhang;Gao Xiang(AVIC Hongdu,Nanchang,Jiangxi,330024)
出处
《教练机》
2021年第2期36-40,共5页
Trainer
关键词
极性测试
并联台
六自由度
Polarity test
Parallel platform
Six-degree-of-freedom