A stochastic sliding mode scheme for longitudinal control of an aircraft model

被引：0
作者：
Khandani, Khosro [1 ]
Majd, Vahid Johari [1 ]
Darestani, Mahdy Rezaei [2 ]
Talebi, Hassan [3 ]
机构：
[1] Tarbiat Modares Univ, Sch Elect & Comp Engn, Intelligent Control Syst Lab, Tehran, Iran
[2] Islamic Azad Univ, Tehran Sci & Res Branch, Sch Aerosp Engn, Dept Mech & Aerosp Engn, Tehran, Iran
[3] Islamic Azad Univ, Tehran Sci & Res Branch, Sch Elect & Comp Engn, Dept Mechatron, Tehran, Iran
来源：
2017 25TH IRANIAN CONFERENCE ON ELECTRICAL ENGINEERING (ICEE) | 2017年
关键词：
Stochastic aircraft model; stochastic sliding mode control; LMI; Guassian noise; reachibility; FRACTIONAL BROWNIAN-MOTION; TIME-DELAY SYSTEMS; H-INFINITY CONTROL; ROBUST STABILIZATION; VARYING DELAY; STABILITY; DESIGN;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
This paper addresses the stochastic sliding mode control problem of an aircraft model given in the literature which is perturbed by Gaussian noise. The objective is to stabilize the decoupled longitudinal dynamics of motion. An integral sliding surface is proposed and the sufficient conditions for stochastic stability of the closed-loop dynamics on the proposed sliding surface are given in terms of linear matrix inequalities (LMIs). The proposed method guarantees the reach ability of the sliding surface, then the tracking error tends to zero in finite time.
引用
收藏
页码：795 / 800
页数：6
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