Adaptive passification-based fault-tolerant flight control

DOI

https://doi.org/10.3182/20070625-5-fr-2916.00122
Final published version

Alexander L. Fradkov
Boris Andrievsky
Dimitri Peaucelle

The adaptive passification-based method is used for fault-tolerant flight control design. Simulation results for HL-20 model and results of experiments with the "LAAS Helicopter Benchmark" are presented, showing efficiency and fault-tolerance of the proposed method.

Original language	English
Title of host publication	ACA' 2007 - 17th IFAC Symposium on Automatic Control in Aerospace - Proceedings
Publisher	International Federation of Automatic Control
Pages	715-720
Number of pages	6
Edition	PART 1
ISBN (Print)	9783902661241
DOIs	https://doi.org/10.3182/20070625-5-fr-2916.00122
State	Published - 2007

Publication series

Name	IFAC Proceedings Volumes (IFAC-PapersOnline)
Number	PART 1
Volume	17
ISSN (Print)	1474-6670

Research areas

Adaptive fault-tolerant flight control, Helicopter control, Passification method

Scopus subject areas

Control and Systems Engineering

ID: 87381825