Conference proceeding
Failure tolerance of sensors in flight control systems in electromagnetic environment
17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267), v 1, pp D51/1-D51/6
1998
Abstract
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).
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Details
- Title
- Failure tolerance of sensors in flight control systems in electromagnetic environment
- Creators
- J Suh - Drexel UniversityB.C ChangA.C Lau
- Publication Details
- 17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267), v 1, pp D51/1-D51/6
- Conference
- 17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference, 17th
- Publisher
- IEEE
- Number of pages
- 6
- Resource Type
- Conference proceeding
- Language
- English
- Academic Unit
- Mechanical Engineering and Mechanics
- Other Identifier
- 991019205312104721