Pitch-decoupled VTOL/FW aircraft: First flights

2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS) Pub Date : 2017-10-01 DOI:10.1109/RED-UAS.2017.8101676

J. Apkarian

引用次数: 7

Abstract

A novel Pitch-Decoupled Tilt Rotor aircraft is introduced that dramatically deviates from all tilt rotor systems developed to date. This new design does not require a complex transition algorithm and is continuously stable and operable in all its rotor pitch configurations.

查看原文本刊更多论文

俯仰解耦VTOL/FW飞机:首飞

介绍了一种新型的俯仰解耦倾斜旋翼飞机，它与迄今为止开发的所有倾斜旋翼系统有很大的不同。这种新设计不需要复杂的转换算法，并且在所有转子螺距配置中都是连续稳定和可操作的。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

求助全文

约1分钟内获得全文求助全文

来源期刊

2017 Workshop on Research, Education and Development of Unmanned Aerial Systems (RED-UAS)

自引率

0.00%

发文量