Fault Tolerant Tracking Control Scheme for UAV Using Dynamic Surface Control Technique

被引：37

作者：

Qian, Moshu ^{[1
,2
]}

Jiang, Bin ^{[1
]}

Xu, Dezhi ^{[1
]}

机构：

[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China

[2] Nanjing Univ Aeronaut & Astronaut, Res Inst UAV, Nanjing 210016, Jiangsu, Peoples R China

来源：

CIRCUITS SYSTEMS AND SIGNAL PROCESSING | 2012年 / 31卷 / 05期

基金：

中国国家自然科学基金;

关键词：

Fault detection; Fault tolerant control; Dynamic surface control; Loss-of-effectiveness (LOE) fault; SPACE-VEHICLE; SYSTEMS; DESIGN;

D O I：

10.1007/s00034-012-9402-5

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：

In this paper, a novel fault tolerant control (FTC) approach is proposed for a hypersonic unmanned aerial vehicle (UAV) attitude dynamical system with actuator loss-of-effectiveness (LOE) fault. Firstly, the nonlinear attitude dynamics of hypersonic UAV is given, which represents the dynamic characteristics of UAV in ascent/reentry phases. Then a fault detection scheme is presented by designing a nonlinear fault detection observer (FDO) for the faulty attitude dynamical system of UAV. Moreover, the fault tolerant control scheme is proposed on the basis of the dynamic surface control technique, which guarantees the asymptotic output tracking and ultimate uniform boundedness of the closed-loop dynamical systems of UAV in the actuator LOE faulty case. Finally, simulation results are given to illustrate the effectiveness of the developed FTC scheme.

引用

页码：1713 / 1729

页数：17

共 27 条

[1] High-order sliding-mode observer for a quadrotor UAV [J].

Benallegue, A. ;

Mokhtari, A. ;

Fridman, L. .

INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2008, 18 (4-5) :427-440

[2] Passive Actuators' Fault-Tolerant Control for Affine Nonlinear Systems [J].

Benosman, M. ;

Lum, K. -Y. .

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2010, 18 (01) :152-163

[3] Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectories [J].

Berend, N ;

Talbot, C .

AEROSPACE SCIENCE AND TECHNOLOGY, 2006, 10 (03) :222-232

[4]

Bollino K.P., AIAA GUID NAV CONTR

[5] Gain-Scheduled Reusable Launch Vehicle Attitude Controller Design [J].

Cui, Nai-gang ;

Xu, Jiangtao ;

Mu, Rongjun ;

Han, Pengxin .

2009 IEEE INTERNATIONAL CONFERENCE ON MECHATRONICS AND AUTOMATION, VOLS 1-7, CONFERENCE PROCEEDINGS, 2009, :4393-4397

[6] Fault-tolerant control for a near space vehicle with a stuck actuator fault based on a Takagi-Sugeno fuzzy model [J].

Gao, Z. ;

Jiang, B. ;

Shi, P. ;

Xu, Y. .

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2010, 224 (I5) :587-598

[7]

Gao ZF, 2010, INT J INNOV COMPUT I, V6, P4843

[8] Fault reconstruction for Lipschitz nonlinear descriptor systems via linear matrix inequality approach [J].

Gao, Zhiwei ;

Ding, Steven X. .

CIRCUITS SYSTEMS AND SIGNAL PROCESSING, 2008, 27 (03) :295-308

[9] Adaptive Fault-Tolerant Tracking Control of Near-Space Vehicle Using Takagi-Sugeno Fuzzy Models [J].

Jiang, Bin ;

Gao, Zhifeng ;

Shi, Peng ;

Xu, Yufei .

IEEE TRANSACTIONS ON FUZZY SYSTEMS, 2010, 18 (05) :1000-1007

[10] Adaptive backstepping fault-tolerant control for flexible spacecraft with unknown bounded disturbances and actuator failures [J].

Jiang, Ye ;

Hu, Qinglei ;

Ma, Guangfu .

ISA TRANSACTIONS, 2010, 49 (01) :57-69

← 1 2 3 →