Uncertainity Estimation Based Approach To Attitude Control of Fixed Wing UAV

被引：5
|
作者：
SaiCharanSagar, Andra [1 ]
Vaitheeswaran, S. M. [1 ]
Shendge, P. D. [2 ]
机构：
[1] Natl Aerosp Labs, Bangalore, Karnataka, India
[2] Coll Engn, Pune, Maharashtra, India
来源：
IFAC PAPERSONLINE | 2016年 / 49卷 / 01期
关键词：
Non linear attitude control; Backstepping(BS); Inertial delay controller(IDC); Fixed wing aircraft;
D O I：
10.1016/j.ifacol.2016.03.066
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The backstepping(BS) algorithm as a promising advanced control lacy has been combined with the inertial delay controller(DC) fat the first buns to handle time varying uncertainties and disturbances for fixed wing unmanned aerial vehicles. Other typical methods like sliding mode controller may need a relatively complex approach to handle uncertainties or under certain conditions may need a complete knowledge of the uncertainty bounds. The stability of overall system of backstepping and inertial delay controller for attitude control is proved and schemes are validated in simulations. (C) 2016, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
引用
收藏
页码：278 / 283
页数：6
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