Event-triggered attitude tracking for rigid spacecraft

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

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

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 languageEnglish
Title of host publicationStudies in Systems, Decision and Control
PublisherSpringer Science and Business Media Deutschland GmbH
Pages183-204
Number of pages22
DOIs
Publication statusPublished - 2021

Publication series

NameStudies in Systems, Decision and Control
Volume356
ISSN (Print)2198-4182
ISSN (Electronic)2198-4190

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