We describe our recent results (2001) related to the design of hybrid online failure detection and identification and adaptive reconfigurable control algorithms for aerial and space vehicles. Our approach is based on the multiple models, switching and tuning methodology and its extensions, and has been demonstrated as an efficient tool for hybrid fault tolerant control under subsystem and component failures and structural damage.
Hybrid fault-tolerant control of aerospace vehicles
2001-01-01
496411 byte
Conference paper
Electronic Resource
English
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