Adaptive Integral Sliding Mode Controller for Longitudinal Rotation Control of a Tilt-Rotor Aircraft

被引：0

作者：

Kim, Jin H. ^{[1
]}

Gadsden, S. Andrew ^{[1
]}

Wilkerson, Stephen A. ^{[2
]}

机构：

[1] Univ Maryland Baltimore Cty, Dept Mech Engn, 1000 Hilltop Circle, Baltimore, MD 21250 USA

[2] York Coll Penn, Dept Comp Sci & Engn, York, PA 17403 USA

来源：

2016 24TH MEDITERRANEAN CONFERENCE ON CONTROL AND AUTOMATION (MED) | 2016年

关键词：

FLIGHT CONTROL;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This paper presents an adaptive integral sliding mode controller for longitudinal rotation control of a tilt-rotor aircraft (TRA). The movable mass, which slides along the wing of the TRA, is considered an unknown disturbance in this paper. The simplified dynamics of the TRA is proposed for the control of the longitudinal rotation during its landing, and application of the adaptive integral sliding mode controller is presented. In the design process of the controller, we applied a sliding surface including an integral term for reinforcing the control performance of the system. This paper compares the results of applying a PID controller and the adaptive integral sliding mode controller with the proposed sliding surface for improved robustness and stability to unknown disturbance.

引用

页码：820 / 825

页数：6

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