Event-triggered attitude tracking for rigid spacecraft

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

*此作品的通讯作者

科研成果: 书/报告/会议事项章节章节同行评审

摘要

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].

源语言英语
主期刊名Studies in Systems, Decision and Control
出版商Springer Science and Business Media Deutschland GmbH
183-204
页数22
DOI
出版状态已出版 - 2021

出版系列

姓名Studies in Systems, Decision and Control
356
ISSN(印刷版)2198-4182
ISSN(电子版)2198-4190

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