Integral-Optimal Sliding Mode Control for Vertical Take-Off and Landing System

被引：4
|
作者：
Aguas, Xavier [1 ]
Revelo, Jefferson [1 ]
Paredes, Israel [1 ]
Cuaycal, Andres [1 ]
Herrera, Marco [1 ]
机构：
[1] Escuela Politec Nacl, Dept Automatizac & Control Ind, Quito, Ecuador
来源：
PROCEEDINGS 3RD INTERNATIONAL CONFERENCE ON INFORMATION SYSTEMS AND COMPUTER SCIENCE (INCISCOS 2018) | 2018年
关键词：
ISMC; VTOL system; ISE; Linear quadratic regulator;
D O I：
10.1109/INCISCOS.2018.00012
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper an Integral Sliding Mode Control (ISMC) based on Linear Quadratic Regulator with Integral action (LQI) as sliding surface for a Vertical Take-Off and Landing (VTOL) System is presented. The main target is check the robustness of ISMC for several experimental tests under parametric uncertainties and external disturbances. The experimental results are compared against LQI controller. In order to validate the proposed controller, the Integral Square Error (ISE) performance index is used. The controllers were implemented on the QNET VTOL trainer.
引用
收藏
页码：29 / 35
页数：7
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