ROBUST CONTROLLER FOR SUPERSONIC UNMANNED AERIAL VEHICLE

被引：1
|
作者：
Burnashev, Vitalii [1 ]
Zbrutsky, Aleksandr [1 ]
机构：
[1] Natl Tech Univ Ukraine, Igor Sikorsky Kyiv Polytech Inst, Dept Aircraft Control Syst, Kiev, Ukraine
来源：
AVIATION | 2019年 / 23卷 / 01期
关键词：
supersonic unmanned aerial vehicle; robust controller; flight trajectory; control quality; transient; controller synthesis; SYSTEM; UAV; DESIGN;
D O I：
10.3846/aviation.2019.10300
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The article is devoted to the synthesis of robust controllers of supersonic unmanned aerial vehicle motion parameters. During the flight, the velocity and altitude of the aircraft varies rapidly within wide limits. Therefore, the required quality of control on each trajectory is provided by a set of dynamic controllers with constant coefficients. The article substantiates the number of such controllers, researches the range of their efficiency. The obtained restrictions on the amplitude-frequency characteristics and weight functions are given. Transients are shown.
引用
收藏
页码：31 / 35
页数：5
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