Controller design for rigid spacecraft attitude tracking with actuator saturation finite-time intercept-angle guidance

Yuanqing Xia; Jinhui Zhang; Kunfeng Lu; Ning Zhou

doi:10.1007/978-981-13-1373-8_9

Controller design for rigid spacecraft attitude tracking with actuator saturation finite-time intercept-angle guidance

Yuanqing Xia^*
, Jinhui Zhang
, Kunfeng Lu
, Ning Zhou

^*此作品的通讯作者

自动化学院

Beijing Aerospace Automatic Control Institute
Fujian Agriculture and Forestry University

科研成果: 书/报告/会议事项章节 › 章节 › 同行评审

摘要

In this chapter, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed, and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception.

源语言	英语
主期刊名	Advances in Industrial Control
出版商	Springer International Publishing
页	171-191
页数	21
DOI	https://doi.org/10.1007/978-981-13-1373-8_9
出版状态	已出版 - 2019

丛书

姓名	Advances in Industrial Control
ISSN（印刷版）	1430-9491
ISSN（电子版）	2193-1577

访问文件

10.1007/978-981-13-1373-8_9

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链接到 Scopus 的出版物

引用此

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title = "Controller design for rigid spacecraft attitude tracking with actuator saturation finite-time intercept-angle guidance",

abstract = "In this chapter, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed, and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception.",

keywords = "Extended State Observer (ESO), Finite-Time Control (FTC), Intercept-Angle Constraint Guidance (IACG), Nonsingular Terminal Sliding Mode Control (NTSMC)",

author = "Yuanqing Xia and Jinhui Zhang and Kunfeng Lu and Ning Zhou",

note = "Publisher Copyright: {\textcopyright} Springer Nature Singapore Pte Ltd 2019.",

year = "2019",

doi = "10.1007/978-981-13-1373-8\_9",

language = "English",

series = "Advances in Industrial Control",

publisher = "Springer International Publishing",

pages = "171--191",

booktitle = "Advances in Industrial Control",

address = "Switzerland",

}

TY - CHAP

T1 - Controller design for rigid spacecraft attitude tracking with actuator saturation finite-time intercept-angle guidance

AU - Xia, Yuanqing

AU - Zhang, Jinhui

AU - Lu, Kunfeng

AU - Zhou, Ning

N1 - Publisher Copyright: © Springer Nature Singapore Pte Ltd 2019.

PY - 2019

Y1 - 2019

N2 - In this chapter, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed, and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception.

AB - In this chapter, new nonsingular terminal sliding mode control guidance laws (NTSMCGLs) to unknown maneuvering target intercept are proposed, and their finite-time convergences are proved. A novel nonsingular terminal sliding mode surface based on a predefined angle is designed to improve intercept performance and avoid singularity problem. The presented guidance law requires no information on maneuvering target that is estimated and compensated by extended state observer (ESO), and it can be used in practical systems where the target can evade freely. Also, undesired chattering is restrained effectively by real-time estimation and compensation of ESO. Simulation results show that the NTSMCGLs can achieve exact interception.

KW - Extended State Observer (ESO)

KW - Finite-Time Control (FTC)

KW - Intercept-Angle Constraint Guidance (IACG)

KW - Nonsingular Terminal Sliding Mode Control (NTSMC)

UR - https://www.scopus.com/pages/publications/85049792281

U2 - 10.1007/978-981-13-1373-8_9

DO - 10.1007/978-981-13-1373-8_9

M3 - Chapter

AN - SCOPUS:85049792281

T3 - Advances in Industrial Control

SP - 171

EP - 191

BT - Advances in Industrial Control

PB - Springer International Publishing

ER -

Controller design for rigid spacecraft attitude tracking with actuator saturation finite-time intercept-angle guidance

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