| An acceleration measurements-based approach for helicopter nonlinear flight control using incremental nonlinear dynamic inversion P Simplício, MD Pavel, E Van Kampen, QP Chu Control Engineering Practice 21 (8), 1065-1077, 2013 | 174 | 2013 |
| Validation of the Beddoes–Leishman dynamic stall model for horizontal axis wind turbines using MEXICO data R Pereira, G Schepers, MD Pavel Wind Energy 16 (2), 207-219, 2013 | 79 | 2013 |
| Adverse rotorcraft pilot couplings—past, present and future challenges MD Pavel, M Jump, B Dang-Vu, P Masarati, M Gennaretti, A Ionita, ... Progress in Aerospace Sciences 62, 1-51, 2013 | 78 | 2013 |
| Adverse rotorcraft-pilot coupling: Recent research activities in Europe O Dieterich, J Götz, B DangVu, H Haverdings, P Masarati, M Pavel, ... 34th European Rotorcraft Forum, 16-19, 2008 | 73 | 2008 |
| Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings–A design perspective MD Pavel, P Masarati, M Gennaretti, M Jump, L Zaichik, B Dang-Vu, L Lu, ... Progress in Aerospace Sciences 76, 55-89, 2015 | 41 | 2015 |
| Understanding the control characteristics of electric vertical take-off and landing (eVTOL) aircraft for urban air mobility MD Pavel Aerospace Science and Technology 125, 107143, 2022 | 37 | 2022 |
| NASA Electric Vertical Takeoff and Landing (eVTOL) Aircraft Technology for Public Services–A White Paper JT Doo, MD Pavel, A Didey, C Hange, NP Diller, MA Tsairides, M Smith, ... | 34 | 2021 |
| Incremental nonlinear dynamic inversion for the apache AH-64 helicopter control MD Pavel, P Shanthakumaran, Q Chu, O Stroosma, M Wolfe, H Cazemier Journal of the American Helicopter Society 65 (2), 1-16, 2020 | 26 | 2020 |
| Adverse rotorcraft-pilot couplings-Prediction and suppression of rigid body RPC; Sketches from the work of GARTEUR HC-AG16 MD Pavel, B Dang Vu, J Götz, M Jump, O Dieterich | 25 | 2008 |
| On the necessary degrees of freedom for helicopter and windturbine low-frequency mode modeling MD Pavel | 23 | 2001 |
| A retrospective survey of adverse rotorcraft pilot couplings in European perspective MD Pavel, J Malecki, BD Vu, P Masarati, M Gennaretti, M Jump, H Smaili, ... The American Helicopter Society 68th Annual Forum, 1-14, 2012 | 21 | 2012 |
| Adverse rotorcraft-pilot coupling: Test campaign development at the university of Liverpool M Jump, S Hodge, B Dang Vu, P Masarati, G Quaranta, M Mattaboni, ... | 21 | 2008 |
| Validation of mathematical models for helicopter flight simulators past, present and future challenges MD Pavel, M White, GD Padfield, G Roth, M Hamers, A Taghizad The Aeronautical Journal 117 (1190), 343-388, 2013 | 20 | 2013 |
| Validation criteria for helicopter real-time simulation models GD Padfield, M Pavel, D Casolaro, G Roth, M Hamers, A Taghizad Sketches from the Work of GARTEUR HC/AG-12. 30th European Rotorcraft Forum …, 2004 | 20 | 2004 |
| Modelling wing wake and tail aerodynamics of a flapping-wing micro aerial vehicle SF Armanini, JV Caetano, CC De Visser, MD Pavel, G De Croon, ... International Journal of Micro Air Vehicles 11, 1756829319833674, 2019 | 19 | 2019 |
| Present and futur trends in rotorcraft pilot couplings (RPCs)-A retrospective survey of recent research activities within the European project ARISTOTEL MD Pavel, J Malecki, B Dang Vu, P Masarati, M Gennaretti, M Jump, ... | 19 | 2011 |
| Understanding the peculiarities of rotorcraft-Pilot-Couplings M Pavel, G Padfield ANNUAL FORUM PROCEEDINGS-AMERICAN HELICOPTER SOCIETY 64 (3), 2018, 2008 | 19 | 2008 |
| Measuring biodynamic feedthrough in helicopters J Venrooij, D Yilmaz, MD Pavel, G Quaranta, M Jump, M Mulder 37th European Rotorcraft Forum (ERF 2011), 958-967, 2012 | 18 | 2012 |
| Adverse rotorcraft-pilot coupling: The construction of the test campaigns at the University of Liverpool M Jump, S Hodge, B Dang Vu, G Masarati, G Quaranta, M Mattaboni, ... 34th European Rotorcraft Forum, 1-19.(2008), 2008 | 18 | 2008 |
| A practical biodynamic feedthrough model for helicopters J Venrooij, MD Pavel, M Mulder, FCT Van Der Helm, HH Bülthoff CEAS Aeronautical Journal 4, 421-432, 2013 | 15 | 2013 |
