Finite-Time Contractive Control of Spacecraft Rendezvous System

被引：1

作者：

Sheng, Jing ^{[1
]}

Geng, Yunhai ^{[1
]}

Li, Min ^{[2
]}

Zhu, Baolong ^{[3
]}

机构：

[1] Harbin Inst Technol, Sch Astronaut, Harbin 150001, Peoples R China

[2] Beijing Inst Control Engn, Beijing 100190, Peoples R China

[3] Qilu Univ Technol, Sch Informat & Automat, Jinan 250353, Peoples R China

来源：

MATHEMATICS | 2023年 / 11卷 / 08期

基金：

中国国家自然科学基金;

关键词：

finite-time contractive stability; state feedback control; spacecraft rendezvous system; cone complementary linearization; C-W equations; STABILIZATION; STABILITY; FEEDBACK; DESIGN;

D O I：

10.3390/math11081871

中图分类号：

O1 [数学];

学科分类号：

0701 ; 070101 ;

摘要：

In this paper we investigate the problem of a finite-time contractive control method for a spacecraft rendezvous control system. The dynamic model of relative motion is formulated by the C-W equations. To improve the convergent performance of the spacecraft rendezvous control system, a finite-time contractive control law is introduced. Lyapunov's direct method is employed to obtain the existence condition of the desired controllers. The controller parameter can be obtained with the help of the cone complementary linearization algorithm. A numerical example verifies the effectiveness of the obtained theoretical results.

引用

页数：14

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