Attitude control using higher order sliding mode

被引：68

作者：

Tiwari, Pyare Mohan ^{[1
]}

Janardhanan, S. ^{[2
]}

Nabi, Mashuq Un ^{[2
]}

机构：

[1] Amity Univ Uttar Pradesh, Dept Elect Engn, Noida, India

[2] Indian Inst Technol, Dept Elect Engn, New Delhi 110016, India

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2016年 / 54卷

关键词：

Attitude control; Higher order sliding mode; Integral sliding mode; Finite-time convergence; VARIABLE-STRUCTURE CONTROL; SYSTEMS; DESIGN;

D O I：

10.1016/j.ast.2016.04.012

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper proposes a chattering-free global finite-time convergent robust control method for the attitude control of a rigid spacecraft. The control method is formulated using higher order sliding mode control in integral sliding mode. The sliding mode order is higher than the system relative degree and therefore, chattering elimination is ensured. In the control design process, unmeasured sliding vector derivative is estimated using a robust exact differentiator. To verify the effectiveness of the proposed control method, simulations are performed in the presence of external disturbances and inertia uncertainty. The proposed controller successfully negates the effect of external disturbances and inertia uncertainty and attitude states attain the desired accuracy with good steady state precision and high convergence speed. (C) 2016 Elsevier Masson SAS. All rights reserved.

引用

页码：108 / 113

页数：6

共 29 条

[1]

[Anonymous], 1978, Spacecraft Attitude Determination and Control

[2] Geometric homogeneity with applications to finite-time stability [J].

Bhat, SP ;

Bernstein, DS .

MATHEMATICS OF CONTROL SIGNALS AND SYSTEMS, 2005, 17 (02) :101-127

[3]

Bhat SP, 1997, P AMER CONTR CONF, P2513, DOI 10.1109/ACC.1997.609245

[4] SLIDING-MODE CONTROLLER-DESIGN FOR SPACECRAFT ATTITUDE TRACKING MANEUVERS [J].

CHEN, YP ;

LO, SC .

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1993, 29 (04) :1328-1333

[5] Stabilization of the attitude of a rigid spacecraft with external disturbances using finite-time control techniques [J].

Ding, Shihong ;

Li, Shihua .

AEROSPACE SCIENCE AND TECHNOLOGY, 2009, 13 (4-5) :256-265

[6] Non-singular terminal sliding mode control of rigid manipulators [J].

Feng, Y ;

Yu, XH ;

Man, ZH .

AUTOMATICA, 2002, 38 (12) :2159-2167

[7] VARIABLE STRUCTURE CONTROL OF NONLINEAR-SYSTEMS - A NEW APPROACH [J].

GAO, WB ;

HUNG, JC .

IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 1993, 40 (01) :45-55

[8] Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control [J].

Jin Erdong ;

Sun Zhaowei .

AEROSPACE SCIENCE AND TECHNOLOGY, 2008, 12 (04) :324-330

[9] Higher order sliding mode control based on integral sliding mode [J].

Laghrouche, Salah ;

Plestan, Franck ;

Glumineau, Alain .

AUTOMATICA, 2007, 43 (03) :531-537

[10] SLIDING ORDER AND SLIDING ACCURACY IN SLIDING MODE CONTROL [J].

LEVANT, A .

INTERNATIONAL JOURNAL OF CONTROL, 1993, 58 (06) :1247-1263

← 1 2 3 →