Design of residual generators and adaptive filters for the FDI of aircraft model sensors

Author:

Castaldi P.,Geri W.,Bonfè M.,Simani S.,Benini M.

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computer Science Applications,Control and Systems Engineering

Reference29 articles.

1. A direct/functional redundancy scheme for fault detection and isolation on an aircraft;Amato;Aerospace Science and Technology,2006

2. Detection of abrupt changes: Theory and application;Basseville,1993

3. Benini, M., Bonfè, M., Castaldi, P., Geri, W., & Simani, S. (2008). Design and performance evaluation of fault diagnosis strategies for a simulated aircraft nonlinear model. Journal of Control Science and Engineering, 1–18 (Special Issue on “Robustness issues in fault diagnosis and fault tolerant control”. Published by Hindawi Publishing Corporation. ISSN (printed): 1687-5249. ISSN (electronic): 1687-5257).

4. Bonfè, M., Castaldi, P., Geri, W., & Simani, S. (2006). Fault detection and isolation for on-board sensors of a general aviation aircraft. International Journal of Adaptive Control and Signal Processing 20(8), 381–408 (Copyright 2006 John Wiley & Sons, Ltd. ISSN: 0890-6327).

5. Design and performance evaluation of residual generators for the FDI of an aircraft;Bonfè;International Journal of Automation and Computing,2007

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