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

^*Corresponding author for this work

School of Automation

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

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.

Original language	English
Title of host publication	Advances in Industrial Control
Publisher	Springer International Publishing
Pages	171-191
Number of pages	21
DOIs	https://doi.org/10.1007/978-981-13-1373-8_9
Publication status	Published - 2019

Publication series

Name	Advances in Industrial Control
ISSN (Print)	1430-9491
ISSN (Electronic)	2193-1577

Keywords

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

Access to Document

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

Cite this

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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",

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address = "Switzerland",

}

Controller design for rigid spacecraft attitude tracking with actuator saturation finite-time intercept-angle guidance. / Xia, Yuanqing ; Zhang, Jinhui; Lu, Kunfeng et al.
Advances in Industrial Control. Springer International Publishing, 2019. p. 171-191 (Advances in Industrial Control).

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

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)

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T3 - Advances in Industrial Control

SP - 171

EP - 191

BT - Advances in Industrial Control

PB - Springer International Publishing

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

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Keywords

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