Event-triggered attitude tracking for rigid spacecraft

Dawei Shi; Yuan Huang; Junzheng Wang; Ling Shi

doi:10.1007/978-981-16-0293-1_8

Event-triggered attitude tracking for rigid spacecraft

Dawei Shi^*, Yuan Huang, Junzheng Wang, Ling Shi

^*Corresponding author for this work

Department of Electronic and Computer Engineering

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

1 Citation (Scopus)

Abstract

In this chapter, we illustrate the applicability of ET-ADRC in attitude tracking for spacecraft systems. Since the kinematic and dynamic equations of rigid spacecraft possess highly coupled nonlinear characteristics and attitude dynamics may suffer from external disturbances, inertia-matrix uncertainties, and even actuator failures, control systems play an important role in achieving attitude maneuvering, attitude tracking, and high-precision pointing of spacecraft, and the attitude-control problem has attracted significant attention over the past few decades [1–5].

Original language	English
Title of host publication	Studies in Systems, Decision and Control
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	183-204
Number of pages	22
DOIs	https://doi.org/10.1007/978-981-16-0293-1_8
Publication status	Published - 2021

Publication series

Name	Studies in Systems, Decision and Control
Volume	356
ISSN (Print)	2198-4182
ISSN (Electronic)	2198-4190

Bibliographical note

Publisher Copyright:
© Science Press 2021.

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10.1007/978-981-16-0293-1_8

Cite this

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abstract = "In this chapter, we illustrate the applicability of ET-ADRC in attitude tracking for spacecraft systems. Since the kinematic and dynamic equations of rigid spacecraft possess highly coupled nonlinear characteristics and attitude dynamics may suffer from external disturbances, inertia-matrix uncertainties, and even actuator failures, control systems play an important role in achieving attitude maneuvering, attitude tracking, and high-precision pointing of spacecraft, and the attitude-control problem has attracted significant attention over the past few decades [1–5].",

author = "Dawei Shi and Yuan Huang and Junzheng Wang and Ling Shi",

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AU - Shi, Dawei

AU - Huang, Yuan

AU - Wang, Junzheng

AU - Shi, Ling

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AB - In this chapter, we illustrate the applicability of ET-ADRC in attitude tracking for spacecraft systems. Since the kinematic and dynamic equations of rigid spacecraft possess highly coupled nonlinear characteristics and attitude dynamics may suffer from external disturbances, inertia-matrix uncertainties, and even actuator failures, control systems play an important role in achieving attitude maneuvering, attitude tracking, and high-precision pointing of spacecraft, and the attitude-control problem has attracted significant attention over the past few decades [1–5].

UR - https://openalex.org/W4242133023

UR - https://www.scopus.com/pages/publications/85102727545

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DO - 10.1007/978-981-16-0293-1_8

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T3 - Studies in Systems, Decision and Control

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EP - 204

BT - Studies in Systems, Decision and Control

PB - Springer Science and Business Media Deutschland GmbH

ER -

Event-triggered attitude tracking for rigid spacecraft

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