In-flight tests of navigation and control system of unmanned aerial vehicle

被引：7
|
作者：
Tomczyk, A [1 ]
机构：
[1] Rzeszow Univ Technol, Fac Mech Engn & Aeronaut, Dept Av & Control, Rzeszow, Poland
来源：
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY | 2003年 / 75卷 / 06期
关键词：
aircraft; flight control; tests and testing;
D O I：
10.1108/00022660310503057
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
In this paper, results of the flight-testing of an unmanned aerial vehicle (UAV) flight control system are presented. APC-4 "SkyGuide" autonomous navigation and control system, designed and developed by the research team of the Department of Avionics and Control at Rzeszow University of Technology, has been tested. Properties of this flight control system, as well as selected results of the in-flight tests conducted on board of the PZL-110 "Koliber" aircraft, are presented. Results obtained confirm that design assumptions of the navigation and control system and research methodology have been appropriate and APC-4 autopilot can be used on UAVs board.
引用
收藏
页码：581 / 587
页数：7
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