2007
DOI: 10.1002/acs.1021
|View full text |Cite
|
Sign up to set email alerts
|

Analysis and detection of incipient faults in post‐fault systems subject to adaptive fault‐tolerant control

Abstract: This paper presents an effective scheme for detecting incipient faults in post-fault systems (PFSs) subject to adaptive fault-tolerant control (AFTC). Through a survey of existing techniques, it is shown that the adaptivity of the AFTC counteracts the effect of an incipient fault in the PFS. This makes some of the conventional fault-detection strategies, such as Beard-Jones detection filters and adaptive observers, ineffective in this situation. It is shown that the unknown input observer (UIO) is an effective… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
23
0

Year Published

2012
2012
2024
2024

Publication Types

Select...
8

Relationship

0
8

Authors

Journals

citations
Cited by 34 publications
(23 citation statements)
references
References 25 publications
0
23
0
Order By: Relevance
“…1 is considered. Each agent is assumed to be a linearised reduced-order aircraft model from [33]. Here the state variables are side-slip angle, roll rate and yaw rate.…”
Section: Simulation Examplementioning
confidence: 99%
“…1 is considered. Each agent is assumed to be a linearised reduced-order aircraft model from [33]. Here the state variables are side-slip angle, roll rate and yaw rate.…”
Section: Simulation Examplementioning
confidence: 99%
“…1. Each agent is assumed to be a linearised reducedorder aircraft model with external disturbance input and mismatched parameter uncertainty from [39]. The dynamics of the ith (i = 0, .…”
Section: Simulation Examplementioning
confidence: 99%
“…, 4) aircraft can be written in the form of (1) and (2), with x i (t) = [p Si (t), p Ri (t), p Yi (t)] T , and u i (t) = [q DTi (t), q AIi (t), q RUi (t), q RTVi (t), q YTVi (t)] T , where p Si (t), p Ri (t), p Yi (t), q DTi (t), q AIi (t), q RUi (t), q RTVi (t) and q YTVi (t) denote respectively side-slip angle, roll rate, yaw rate, differential tail deflection, aileron deflection, rudder deflection, roll thrust vector deflection and yaw thrust vector deflection, respectively. As done in [39], angle of attack is equal to 29 The revolution of controller parametersα ij (t),k i2 (t),k i3 (t),k i4 (t), i = 1, . .…”
Section: Simulation Examplementioning
confidence: 99%
“…Replacing () xk and () fk of 0 () yk in (1) with the estimated ˆ() xk and ˆ( ) fk in (19), respectively, then we obtain the reconstructed delay-free output 0 () yk of kth instant of (11). Replacing () xk of (5) …”
Section: Physically Realizable Fault-tolerant Controlmentioning
confidence: 99%
“…In [10], a post fault tolerant control approach was proposed for sensor fault of an induction motor and validated by an experiment of induction motor. For a stuck-actuator fault, [11] presented an adaptive fault-tolerant control approach to accommodate the incipient faults. Another adaptive fault-tolerant control scheme was proposed in [12] based on leader-follower consensus control when actuator faults occurred.…”
Section: Introductionmentioning
confidence: 99%