Event-triggered attitude tracking for rigid spacecraft

被引：13

作者：

Cai, Deheng ^{[1
]}

Zou, Hengguang ^{[1
,2
]}

Wang, Junzheng ^{[1
]}

Huang, Yuan ^{[1
]}

Shi, Dawei ^{[1
]}

机构：

[1] Beijing Inst Technol, Sch Automat, State Key Lab Intelligent Control & Decis Complex, Beijing 100081, Peoples R China

[2] China Acad Space Technol, Beijing 100094, Peoples R China

来源：

SCIENCE CHINA-INFORMATION SCIENCES | 2019年 / 62卷 / 12期

基金：

中国国家自然科学基金;

关键词：

spacecraft; attitude tracking; active disturbance rejection control; event-triggered control; extended state observer; DISTURBANCE REJECTION CONTROL; ADAPTIVE-CONTROL;

D O I：

10.1007/s11432-018-9844-3

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 study aims to investigate the problem of attitude control for a spacecraft with inertial uncertainties, external disturbances, and communication restrictions. An event-triggered active disturbance rejection control approach is proposed for attitude tracking of the spacecraft. An event-triggered mechanism is introduced together with an extended state observer to jointly monitor the system states and total disturbances. The observation error is proved to be uniformly bounded. Based on the proposed control scheme, the integrated tracking system is shown to be asymptotically stable, implying successful attitude tracking of the spacecraft for the desired motion. Numerical results illustrate the effectiveness of the control strategy in achieving satisfactory tracking performance with a reduced data-transmission cost.

引用

页数：16

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