Author:
Kosyanchuk V.,Zheltov S.,Zybin E.
Abstract
Abstract
The concept of an intelligent hybrid aircraft fault-tolerant flight control system operating under complete parametric and structural uncertainty is considered. Fault tolerance in the proposed system is ensured through the efficient integration of model-based and model-free health monitoring and reconfiguring methods.
Subject
General Physics and Astronomy
Cited by
4 articles.
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