|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
|Adverse rotorcraft-pilot coupling: Recent research activities in Europe|
O Dieterich, J Götz, B Dang Vu, H Haverdings, P Masarati, M Pavel, ...
|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
|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
|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
|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
|On the necessary degrees of freedom for helicopter and wind turbine low-frequency mode modeling|
|A retrospective survey of adverse rotorcraft pilot couplings in European perspective|
M Pavel, J Malecki, B Dang Vu, P Masarati, M Gennaretti, M Jump, ...
68th International Annual Forum American Helicopter Society (AHS), 2238-2251, 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, ...
|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, ...
Royal Aeronautical Society, 2008
|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, ...
|Measuring biodynamic feedthrough in helicopters|
J Venrooij, D Yilmaz, MD Pavel, G Quaranta, M Jump, M Mulder
|Understanding the peculiarities of rotorcraft, pilot, couplings|
MD Pavel, GD Padfield
Proceedings of the 64th Annual forum of the American Helicopter Society, p …, 2008
|Validation Criteria for Helicopter Real-time Simulation Models-Sketches from the Work of Garteur HC-AG12|
GD Padfield, D Casolaro, M Hamers, M Pavel, G Roth, A Taghizad
|A practical biodynamic feedthrough model for helicopters|
J Venrooij, MD Pavel, M Mulder, FCT Van Der Helm, HH Bülthoff
CEAS Aeronautical Journal 4 (4), 421-432, 2013
|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
|Present and future trends in aircraft and rotorcraft pilot couplings—a retrospective survey of recent research activities within the European project ARISTOTEL|
MD Pavel, J Malecki, B DangVu, P Masarati, M Gennaretti, M Jump, ...
37th European Rotorcraft Forum, 13-15, 2011
|Aircraft and rotorcraft pilot coupling: a survey of recent research activities within the European project ARISTOTEL|
M Pavel, J Malecki, B Dang Vu, P Masarati, G Quaranta, M Gennaretti, ...
3rd CEAS Air & Space Conference and 21st AIDAA Congress, 1937-1959, 2011
|Fidelity of helicopter real-time models|
GD Padfield, M Pavel, D Casolaro, G Roth, M Hamers, A Taghizad
Proc. 61st Annual Forum of the American Helicopter Society, Grapevine, Texas, 2005
|A review of rotorcraft wake modeling methods for flight dynamics applications|
WRM Van Hoydonck, H Haverdings, MD Pavel