2010
DOI: 10.1007/978-3-642-11690-2_4
|View full text |Cite
|
Sign up to set email alerts
|

Real-Time Identification of Aircraft Physical Models for Fault Tolerant Flight Control

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1

Citation Types

0
2
0

Year Published

2019
2019
2023
2023

Publication Types

Select...
2
2

Relationship

0
4

Authors

Journals

citations
Cited by 4 publications
(2 citation statements)
references
References 11 publications
0
2
0
Order By: Relevance
“…However, due to the significant changes that may take place as a consequence of failure, the aerodynamic model of the aircraft will obviously be different from the nominal one. In order to enhance the capabilities of automatic flight control systems, failures will have to be detected and identified on board during the flight in real-time (Chu et al, 2010).…”
Section: Increasing Validity By Fault-tolerant Techniquesmentioning
confidence: 99%
“…However, due to the significant changes that may take place as a consequence of failure, the aerodynamic model of the aircraft will obviously be different from the nominal one. In order to enhance the capabilities of automatic flight control systems, failures will have to be detected and identified on board during the flight in real-time (Chu et al, 2010).…”
Section: Increasing Validity By Fault-tolerant Techniquesmentioning
confidence: 99%
“…The model-based fault detection, isolation, and reconfiguration method is divided into the fault detection and isolation step, and the controller reconfiguration step [61]. The "Golden Rules" to design a fault-tolerant aircraft include: hardware redundancy, monitoring of flight control elements in real-time, reconfiguration in case of failure, dissimilarity, installation segregation, and robustness of software and system equipment [62], [63].…”
Section: B Run-time Control and Middlewarementioning
confidence: 99%