Adaptive global prescribed performance control for rigid spacecraft subject to angular velocity constraints and input saturation

This article investigates the prescribed performance attitude tracking control issue of rigid spacecraft subject to angular velocity constraints, input saturation, actuator failures, external disturbances and inertia uncertainty. With the aid of a shifting function, we propose the global asymmetrica...

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Bibliographic Details
Published inNonlinear dynamics Vol. 111; no. 23; pp. 21691 - 21705
Main Authors Su, Yuhan, Shen, Shaoping
Format Journal Article
LanguageEnglish
Published Dordrecht Springer Netherlands 01.12.2023
Springer Nature B.V
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