Codice QR

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...

Descrizione completa

Salvato in:
Dettagli Bibliografici
Autori principali: Milad Azimi, Marzieh Eghlimi Dezh
Natura: Artigo
Lingua:Persa
Pubblicazione: Iranian Space Research Institute 2025-02-01
Serie:علوم، فناوری و کاربردهای فضایی
Soggetti:
Accesso online:https://journal.isrc.ac.ir/article_216285_57d51a892f30d93100ec2f21f36de7ce.pdf
Tags: Aggiungi Tag
Nessun Tag, puoi essere il primo ad aggiungerne!!