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
01.01.2001
496411 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A fault tolerant implementation for aerospace
AIAA | 1993
|A Fault Tolerant Implementation for Aerospace
British Library Conference Proceedings | 1993
|A dual, fault-tolerant aerospace actuator
NTRS | 1985
|