Fixed-Time Attitude Tracking Control for Spacecraft With Input Quantization

被引：128

作者：

Sun, Haibin ^{[1
]}

Hou, Linlin ^{[2
]}

Zong, Guangdeng ^{[1
]}

Yu, Xinghuo ^{[3
]}

机构：

[1] Qufu Normal Univ, Sch Engn, Rizhao 276826, Shandong, Peoples R China

[2] Qufu Normal Univ, Sch Informat Sci & Engn, Rizhao 276826, Shandong, Peoples R China

[3] RMIT, Sch Engn, Melbourne, Vic 3000, Australia

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2019年 / 55卷 / 01期

基金：

澳大利亚研究理事会; 中国国家自然科学基金;

关键词：

SLIDING MODE CONTROL; NONLINEAR-SYSTEMS; CONTROL DESIGN; STABILIZATION;

D O I：

10.1109/TAES.2018.2849158

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper investigates the fixed-time attitude tracking control problem for rigid spacecraft with input quantization and external disturbances. A novel fixed-time disturbance observer is designed to estimate unknown disturbances. By using adding a power integrator technique, a fixed-time controller is constructed, which can guarantee system states converge to a neighborhood of origin in fixed time. The parameter of quantizer can be coarsely chosen. Finally, simulation results are employed to demonstrate the effectiveness of the developed control scheme.

引用

页码：124 / 134

页数：11

共 32 条

[1] Backstepping Control Design with Actuator Torque Bound for Spacecraft Attitude Maneuver [J].

Ali, Imran ;

Radice, Gianmarco ;

Kim, Jongrae .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (01) :254-259

[2] Multivariable continuous fixed-time second-order sliding mode control: design and convergence time estimation [J].

Basin, Michael ;

Panathula, Chandrasekhara Bharath ;

Shtessel, Yuri .

IET CONTROL THEORY AND APPLICATIONS, 2017, 11 (08) :1104-1111

[3] Adaptive uniform finite-/fixed-time convergent second-order sliding-mode control [J].

Basin, Michael ;

Panathula, Chandrasekhara Bharath ;

Shtessel, Yuri .

INTERNATIONAL JOURNAL OF CONTROL, 2016, 89 (09) :1777-1787

[4] Attitude Synchronization for Flexible Spacecraft With Communication Delays [J].

Du, Haibo ;

Li, Shihua .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2016, 61 (11) :3625-3630

[5] Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization [J].

Du, Haibo ;

Li, Shihua ;

Qian, Chunjiang .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2011, 56 (11) :2711-2717

[6] Geometric Approach to Spacecraft Attitude Control Using Magnetic and Mechanical Actuation [J].

Forbes, James Richard ;

Damaren, Christopher John .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (02) :590-595

[7]

Hardy J. Littlewood, 1952, The Mathematical Gazette, DOI DOI 10.1017/S0025557200027455

[8] Fixed-Time Rendezvous Control of Spacecraft With a Tumbling Target Under Loss of Actuator Effectiveness [J].

Jiang, Boyan ;

Hu, Qinglei ;

Friswell, Michael I. .

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2016, 52 (04) :1576-1586

[9] Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults [J].

Jiang, Boyan ;

Hu, Qinglei ;

Friswell, Michael I. .

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2016, 24 (05) :1892-1898

[10] Global set stabilization of the spacecraft attitude control problem based on quaternion [J].

Li, Shihua ;

Ding, Shihong ;

Li, Qi .

INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2010, 20 (01) :84-105

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