电磁环境下飞行控制系统传感器的故障容忍度

17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267) Pub Date : 1998-10-31 DOI:10.1109/DASC.1998.741551

J. Suh, B. Chang, A. Lau

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摘要

在飞行控制系统中，高强度辐射场(HIRE)条件可能导致传感器和/或控制器失效。为了建立电磁环境下传感器的容错能力，提出了一种飞行动力学仿真方案。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Failure tolerance of sensors in flight control systems in electromagnetic environment

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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17th DASC. AIAA/IEEE/SAE. Digital Avionics Systems Conference. Proceedings (Cat. No.98CH36267)

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