| Lithium-ion Open Circuit Voltage (OCV) curve modelling and its ageing adjustment L Lavigne, J Sabatier, JM Francisco, F Guillemard, A Noury Journal of Power Sources 324, 694-703, 2016 | 141 | 2016 |
| Lithium-ion batteries modeling: A simple fractional differentiation based model and its associated parameters estimation method J Sabatier, JM Francisco, F Guillemard, L Lavigne, M Moze, M Merveillaut Signal Processing 107, 290-301, 2015 | 62 | 2015 |
| Oscillatory failure case detection for new generation Airbus aircraft: a model-based challenge L Lavigne, A Zolghadri, P Goupil, P Simon 2008 47th IEEE Conference on Decision and Control, 1249-1254, 2008 | 26 | 2008 |
| Nonlinear observer-based OFC detection for A380 aircraft EA Garcia, A Zolghadri, P Goupil, L Lavigne, P Simon IFAC Proceedings Volumes 42 (8), 47-52, 2009 | 25 | 2009 |
| Robust and early detection of oscillatory failure case for new generation Airbus aircraft L Lavigne, A Zolghadri, P Goupil, P Simon AIAA Guidance, Navigation and Control Conference and Exhibit, 7139, 2008 | 24 | 2008 |
| A model-based technique for early and robust detection of oscillatory failure case in A380 actuators L Lavigne, A Zolghadri, P Goupil, P Simon International Journal of Control, Automation and Systems 9 (1), 42-49, 2011 | 22 | 2011 |
| Outils d'analyse et de synthèse des lois de commande robuste des systèmes dynamiques plats. L Lavigne Université Sciences et Technologies-Bordeaux I, 2003 | 20 | 2003 |
| Modelling of longitudinal disturbed aircraft model by flatness approach B Bergeon, LL Lavigne, F Cazaurang 2003 AIAA Guidance, Navigation, and Control Conference and Exhibit, 2003 | 20 | 2003 |
| Method and device for detecting oscillatory failures in a position servocontrol subsystem of an aircraft control surface P Goupil, A Zolghadri, L Lavigne US Patent 8,160,770, 2012 | 19 | 2012 |
| Fault detection and isolation on a three tank system using differential flatness CM Torres, L Lavigne, F Cazaurang, EA García, DD Romero 2013 European Control Conference (ECC), 2433-2438, 2013 | 18 | 2013 |
| A genetic fuzzy logic based approach to solving the aircraft conflict resolution problem A Sathyan, N Ernest, L Lavigne, F Cazaurang, M Kumar, K Cohen AIAA Information Systems-AIAA Infotech@ Aerospace, 1751, 2017 | 16 | 2017 |
| New sequential probability ratio test: Validation on A380 flight data L Lavigne, F Cazaurang, L Fadiga, P Goupil Control Engineering Practice 22, 1-9, 2014 | 16 | 2014 |
| Satellite path planning by flatness approach F Cazaurang, L Lavigne International Review of Aerospace Engineering 2 (3), 123-132, 2009 | 15 | 2009 |
| Lithium-ion battery state of charge estimation using a fractional battery model JM Francisco, J Sabatier, L Lavigne, F Guillemard, M Moze, M Tari, ... ICFDA'14 International Conference on Fractional Differentiation and Its …, 2014 | 14 | 2014 |
| Modeling of disturbed flat system for robust control design L Lavigne, F Cazaurang, B Bergeon IFAC Proceedings Volumes 34 (6), 759-762, 2001 | 13 | 2001 |
| Fault tolerant control of a three tank system: A flatness based approach CM Torres, L Lavigne, F Cazaurang, EA García, DD Romero 2013 Conference on Control and Fault-Tolerant Systems (SysTol), 529-534, 2013 | 12 | 2013 |
| Flatness-based fault tolerant control C Martínez-Torres, L Lavigne, F Cazaurang, E Alcorta-García, ... Dyna 81 (188), 131-138, 2014 | 10 | 2014 |
| Convertible aircraft dynamic modelling and flatness analysis TB Airimitoaie, GP Aguilar, L Lavigne, C Farges, F Cazaurang IFAC-PapersOnLine 51 (2), 25-30, 2018 | 8 | 2018 |
| Robust and early detection of oscillatory failure case for new generation airbus L Lavigne, A Zolghadri, P Goupil, P Simon AIAA Guidance, Navigation and Control Conference and Exhibit, 2008 | 7 | 2008 |
| Modeling a disturbed simplified aircraft model with flatness property L Lavigne, F Cazaurang, B Bergeon Proceeding of AIAA Guidance, Navigation and Control Conference, Texas, Austin, 2003 | 7 | 2003 |
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