| Development of linear-parameter-varying models for aircraft A Marcos, GJ Balas Journal of Guidance, Control, and Dynamics 27 (2), 218-228, 2004 | 451 | 2004 |
| Reconfigurable LPV control design for Boeing 747-100/200 longitudinal axis S Ganguli, A Marcos, G Balas Proceedings of the 2002 American control conference (IEEE cat. no. CH37301 …, 2002 | 158 | 2002 |
| An application of H∞ fault detection and isolation to a transport aircraft A Marcos, S Ganguli, GJ Balas Control Engineering Practice 13 (1), 105-119, 2005 | 155 | 2005 |
| Fault reconstruction using a LPV sliding mode observer for a class of LPV systems H Alwi, C Edwards, A Marcos Journal of the Franklin Institute 349 (2), 510-530, 2012 | 102 | 2012 |
| Linear parameter varying modeling of the Boeing 747-100/200 longitudinal motion A Marcos, G Balas AIAA Guidance, Navigation, and Control Conference and Exhibit, 4347, 2001 | 97 | 2001 |
| A robust integrated controller/diagnosis aircraft application A Marcos, GJ Balas International Journal of Robust and Nonlinear Control: IFAC‐Affiliated …, 2005 | 88 | 2005 |
| Linear paramater-varying detection filter design for a boeing 747-100/200 aircraft I Szászi, A Marcos, GJ Balas, J Bokor Journal of guidance, control, and dynamics 28 (3), 461-470, 2005 | 84 | 2005 |
| An overview of the FP7 RECONFIGURE project: industrial, scientific and technological objectives P Goupil, J Boada-Bauxell, A Marcos, P Rosa, M Kerr, L Dalbies IFAC-PapersOnLine 48 (21), 976-981, 2015 | 71 | 2015 |
| AIRBUS efforts towards advanced real-time fault diagnosis and fault tolerant control P Goupil, J Boada-Bauxell, A Marcos, E Cortet, M Kerr, H Costa IFAC Proceedings Volumes 47 (3), 3471-3476, 2014 | 69 | 2014 |
| A Boeing 747-100/200 aircraft fault tolerant and fault diagnostic benchmark A Marcos, GJ Balas University of Minnesota, Minneapolis, MN, Technical Report AEM-UoM-2003-1, 2003 | 69 | 2003 |
| Advanced diagnosis for sustainable flight guidance and control: The European ADDSAFE project P Goupil, A Marcos SAE technical paper, 2011 | 54 | 2011 |
| The European ADDSAFE project: Industrial and academic efforts towards advanced fault diagnosis P Goupil, A Marcos Control Engineering Practice 31, 109-125, 2014 | 52 | 2014 |
| Structured singular-value analysis of the VEGA launcher in atmospheric flight P Simplicio, S Bennani, A Marcos, C Roux, X Lefort Journal of Guidance, Control, and Dynamics 39 (6), 1342-1355, 2016 | 49 | 2016 |
| Guidance of reusable launchers: improving descent and landing performance P Simplício, A Marcos, S Bennani Journal of Guidance, Control, and Dynamics 42 (10), 2206-2219, 2019 | 47 | 2019 |
| Reusable launchers: development of a coupled flight mechanics, guidance, and control benchmark P Simplício, A Marcos, S Bennani Journal of Spacecraft and Rockets 57 (1), 74-89, 2020 | 43 | 2020 |
| Robustness analysis of a reusable launch vehicle flight control law PP Menon, I Postlethwaite, S Bennani, A Marcos, DG Bates Control Engineering Practice 17 (7), 751-765, 2009 | 41 | 2009 |
| Industrial benchmarking and evaluation of ADDSAFE FDD designs P Goupil, A Marcos IFAC Proceedings Volumes 45 (20), 1131-1136, 2012 | 36 | 2012 |
| Flight testing of an structured H-infinity controller: An EU-Japan collaborative experience A Marcos, M Sato 2017 IEEE Conference on Control Technology and Applications (CCTA), 2132-2137, 2017 | 34 | 2017 |
| LPV modeling, analysis and design in space systems: Rationale, objectives and limitations A Marcos, S Bennani AIAA guidance, navigation, and control conference, 5633, 2009 | 34 | 2009 |
| Flight control design for a highly flexible flutter demonstrator T Luspay, D Ossmann, M Wuestenhagen, D Teubl, T Baár, M Pusch, ... AIAA Scitech 2019 Forum, 1817, 2019 | 33 | 2019 |
Andrea IannelliAssistant Professor, University of Stuttgart在 ist.uni-stuttgart.de 的电子邮件经过验证
