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Aircraft flight control system fault tolerance under structural and parametric uncertainties
Author(s) -
Vladislav Kosyanchuk,
Sergey Yu. Zheltov,
E. Yu. Zybin
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1864/1/012005
Subject(s) - parametric statistics , fault tolerance , control (management) , computer science , control engineering , fault (geology) , control system , engineering , reliability engineering , artificial intelligence , statistics , mathematics , electrical engineering , seismology , geology
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.

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