High Intensity Radiated Field (HIRE) conditions may cause sensor and/or controller failure in flight control system. In this paper, a flight dynamics imitation scheme is proposed to establish the failure tolerance of sensors in Electro-Magnetic Environment (EME).
Failure tolerance of sensors in flight control systems in electromagnetic environment
17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267) ; 1 ; D51/1-D51/6 vol.1
01.01.1998
411997 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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