Attitude Control of Fixed Wing UAV using Multiple Sliding Surface

被引：0
|
作者：
Sagar, Andra Saicharan [1 ]
Shendge, P. D. [2 ]
Vaitheeswaran, S. M. [3 ]
机构：
[1] Coll Engn, Nat Aerosp Labs, Pune, Maharashtra, India
[2] Coll Engn, Dept Instrumentat & Control, Pune, Maharashtra, India
[3] CSIR, Natl Aerosp Labs, Aerosp Elect & Syst Div, Bangalore, Karnataka, India
来源：
PROCEEDINGS OF THE FIRST IEEE INTERNATIONAL CONFERENCE ON POWER ELECTRONICS, INTELLIGENT CONTROL AND ENERGY SYSTEMS (ICPEICES 2016) | 2016年
关键词：
Fixed Wing Unmanned Aircraft; Sliding Mode Controller (SMC); Multiple Sliding Surface Controller (MSSC); Inertial Delay Controller (IDC); FLIGHT CONTROL; SYSTEMS;
D O I：
暂无
中图分类号：
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号：
0807 ; 0820 ;
摘要：
A design method for controlling the attitude of a fixed wing aircraft in the presence of uncertainties is proposed in the Multiple Sliding Surface framework. Inertial Delay Controller is integrated with Multiple Sliding surface Controller to increase the performance of system by estimating the uncertainties that are present in the system.
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页数：6
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