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A note on interval observer design for unknown input estimation

International journal of control, 2016-01, Vol.89 (1), p.25-37

2016

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A review of fault management issues in aircraft systems: Current status and future directions

Progress in aerospace sciences, 2024-05, Vol.147, p.101008, Article 101008

Zolghadri, A.

2024

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Design and analysis of robust residual generators for systems under feedback control

Automatica (Oxford), 2005-02, Vol.41 (2), p.251-264

2005

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H ∞ ∕ H − LPV solutions for fault detection of aircraft actuator faults: Bridging the gap between theory and practice

International journal of robust and nonlinear control, 2015-03, Vol.25 (5), p.649-672

2015

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Actuator fault detection and compensation under feedback control

Automatica (Oxford), 2011-08, Vol.47 (8), p.1699-1705

2011

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Fault tolerant flight control: from theory to piloted flight simulator experiments

IET control theory & applications, 2010-08, Vol.4 (8), p.1451-1464

2010

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Non-minimum phase switched systems: HOSM-based fault detection and fault identification via Volterra integral equation

International journal of adaptive control and signal processing, 2014-12, Vol.28 (12), p.1372-1397

2014

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Design of fault diagnosis filters: A multi-objective approach

Journal of the Franklin Institute, 2005-07, Vol.342 (4), p.421-446

2005

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Interval State Estimation for a Class of Nonlinear Systems

IEEE transactions on automatic control, 2012-01, Vol.57 (1), p.260-265

2012

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Fault tolerant controller for a class of additive faults: a quasi-continuous high-order sliding mode approach

Journal of physics. Conference series, 2015, Vol.659 (1), p.12005

2015

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Control of Nonlinear and LPV Systems: Interval Observer-Based Framework

IEEE transactions on automatic control, 2013-03, Vol.58 (3), p.773-778

2013

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Early warning and prediction of flight parameter abnormalities for improved system safety assessment

Reliability engineering & system safety, 2002-04, Vol.76 (1), p.19-27

Zolghadri, A.

2002

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Coupled linear parameter varying and flatness-based approach for space re-entry vehicles guidance

IET control theory & applications, 2009-08, Vol.3 (8), p.1081-1090

2009

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Adaptive nonlinear state-space modelling for the prediction of daily mean PM10 concentrations

Environmental modelling & software : with environment data news, 2006-06, Vol.21 (6), p.885-894

2006

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Fault tolerant multi-sensor data fusion for autonomous navigation in future civil aviation operations

Control engineering practice, 2022-06, Vol.123 (5), p.105132, Article 105132

2022

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An algorithm for real-time failure detection in Kalman filters

IEEE transactions on automatic control, 1996-10, Vol.41 (10), p.1537-1539

Zolghadri, A.

1996

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Development of an operational model-based warning system for tropospheric ozone concentrations in Bordeaux, France

Environmental modelling & software : with environment data news, 2004-04, Vol.19 (4), p.369-382

2004

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A redundancy-based strategy for safety management in a modern civil aircraft

Control engineering practice, 2000, Vol.8 (5), p.545-554

Zolghadri, A.

2000

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Fault tolerant multi-sensor data fusion for autonomous navigation in future civil aviation operations

Control engineering practice, 2022-06, Vol.123

2022

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Symbolic Observer-Based Controller for Uncertain Nonlinear Systems

IEEE control systems letters, 2021-10, Vol.5 (4), p.1297-1302

2021

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Minimax statistical models for air pollution time series. Application to ozone time series data measured in Bordeaux

Environmental monitoring and assessment, 2004-11, Vol.98 (1-3), p.275-294

2004

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Off-line robust fault diagnosis using the generalized structured singular value

Automatica (Oxford), 2002-08, Vol.38 (8), p.1347-1358

2002

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A non-conservative H−/H∞ solution for early and robust fault diagnosis in aircraft control surface servo-loops

Control engineering practice, 2014-10, Vol.31, p.183-199

2014

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Abstraction-based control synthesis using partial information

European journal of control, 2022-01, Vol.63, p.214-222

2022

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Design of Robust Fault Detection Filters for Multivariable Feedback Systems

International journal of modelling & simulation, 2006-01, Vol.26 (1), p.17-26

2006

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A note on interval observer design for unknown input estimation

A review of fault management issues in aircraft systems: Current status and future directions

Design and analysis of robust residual generators for systems under feedback control

H ∞ ∕ H − LPV solutions for fault detection of aircraft actuator faults: Bridging the gap between theory and practice

Actuator fault detection and compensation under feedback control

Fault tolerant flight control: from theory to piloted flight simulator experiments

Non-minimum phase switched systems: HOSM-based fault detection and fault identification via Volterra integral equation

Design of fault diagnosis filters: A multi-objective approach

Interval State Estimation for a Class of Nonlinear Systems

Fault tolerant controller for a class of additive faults: a quasi-continuous high-order sliding mode approach

Control of Nonlinear and LPV Systems: Interval Observer-Based Framework

Early warning and prediction of flight parameter abnormalities for improved system safety assessment

Coupled linear parameter varying and flatness-based approach for space re-entry vehicles guidance

Adaptive nonlinear state-space modelling for the prediction of daily mean PM10 concentrations

Fault tolerant multi-sensor data fusion for autonomous navigation in future civil aviation operations

An algorithm for real-time failure detection in Kalman filters

Development of an operational model-based warning system for tropospheric ozone concentrations in Bordeaux, France

A redundancy-based strategy for safety management in a modern civil aircraft

Fault tolerant multi-sensor data fusion for autonomous navigation in future civil aviation operations

Symbolic Observer-Based Controller for Uncertain Nonlinear Systems

Minimax statistical models for air pollution time series. Application to ozone time series data measured in Bordeaux

Off-line robust fault diagnosis using the generalized structured singular value

A non-conservative H−/H∞ solution for early and robust fault diagnosis in aircraft control surface servo-loops

Abstraction-based control synthesis using partial information

Design of Robust Fault Detection Filters for Multivariable Feedback Systems

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