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Adaptive Integral Fault-Tolerant Sliding Mode Control of a Flexible Spacecraft Based on Disturbance Observer

This article investigates the enhancement of the control performance of flexible spacecraft by addressing actuator faults, input saturations, and internal and external disturbances (including flexible solar panel vibrations) during attitude maneuvers. First, the proposed disturbance observer, which...

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Detalles Bibliográficos
Principais autores: Milad Azimi, Marzieh Eghlimi Dezh
Formato: Artigo
Idioma:Persa
Publicado: Iranian Space Research Institute 2025-02-01
Series:علوم، فناوری و کاربردهای فضایی
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Acceso en liña:https://journal.isrc.ac.ir/article_216285_57d51a892f30d93100ec2f21f36de7ce.pdf
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