Envelop Expansion Flight Test of Flight Control Systems for TR-60 Tilt-rotor UAV

被引：0

作者：

Kang, Young-Shin ^{[1
]}

Park, Bum-Jin ^{[1
]}

Cho, Am ^{[1
]}

Yoo, Chang-sun ^{[1
]}

Chois, Seong-wook ^{[1
]}

机构：

[1] Korea Aerosp Res Inst, Unmanned Aircraft Syst Div, Taejon 305806, South Korea

来源：

2013 13TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS 2013) | 2013年

关键词：

flight test; tilt-rotor; flight control; anomalies; trouble shooting; unmanned air vehicle (UAV); operational flight program (OFP);

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Flight tests of TR-60 in order to evaluate the control performance in helicopter, conversion and airplane mode were completed. In order to reduce the development risk and schedule, single channel out of the dual flight control computer of Smart UAV (TR-100) was used without the other modification. Therefore the operational flight program (OFP) had the minimum changes only on control laws. Even though similar flight control system was applied to the scaled tilt-rotor aircraft, named as TR-60, many unexpected anomalies occurred during flight test from hover to airplane mode mainly due to the different bandwidth between TR-100 and TR-60. This paper presented the details of flight test data and anomalies which occurred durirlg flight test of TR-60 as well as the trouble shooting results.

引用

页码：1866 / 1871

页数：6