Linearized aeroservoelastic analysis of rotor-wing aircraft P Masarati, V Muscarello, G Quaranta | 30 | 2010 |
An integrated environment for helicopter aeroservoelastic analysis: the ground resonance case P Masarati, V Muscarello, G Quaranta, A Locatelli, D Mangone, L Riviello, ... | 24 | 2011 |
Rotorcraft aeroelastic stability using robust analysis G Quaranta, A Tamer, V Muscarello, P Masarati, M Gennaretti, J Serafini, ... CEAS Aeronautical Journal 5 (1), 29-39, 2014 | 18 | 2014 |
The role of rotor coning in helicopter proneness to collective bounce V Muscarello, G Quaranta, P Masarati Aerospace Science and Technology 36, 103-113, 2014 | 15 | 2014 |
Prediction and simulator verification of roll/lateral adverse aeroservoelastic rotorcraft–pilot couplings V Muscarello, G Quaranta, P Masarati, L Lu, M Jones, M Jump Journal of Guidance, Control, and Dynamics 39 (1), 42-60, 2016 | 14 | 2016 |
Multibody analysis of rotorcraft-pilot coupling V Muscarello, P Masarati, G Quaranta, P Eberhard, P Ziegler 2nd joint international conference on multibody system dynamics, Stuttgart …, 2012 | 14 | 2012 |
Lead-lag damper robustness analysis for helicopter ground resonance G Quaranta, V Muscarello, P Masarati Journal of Guidance, Control, and Dynamics 36 (4), 1150-1161, 2013 | 13 | 2013 |
Aerodynamic models for cycloidal rotor analysis L Gagnon, M Morandini, G Quaranta, V Muscarello, P Masarati Aircraft Engineering and Aerospace Technology: An International Journal, 2016 | 12 | 2016 |
Robust aeroservoelastic stability of helicopters: application to the air/ground resonance P Masarati, V Muscarello, G Quaranta 67th International Annual Forum American Helicopter Society (AHS), 1191-1201, 2011 | 10 | 2011 |
Robust aeroservoelastic analysis for the investigation of rotorcraft pilot couplings V Muscarello, P Masarati, G Quaranta 3rd CEAS Air & Space Conference and 21st AIDAA Congress, 639-650, 2011 | 9 | 2011 |
Feasibility assessment: a cycloidal rotor to replace conventional helicopter technology L Gagnon, M Morandini, G Quaranta, V Muscarello, P Masarati, ... | 8 | 2014 |
Cyclogyro thrust vectoring for anti-torque and control of helicopters L Gagnon, M Morandini, G Quaranta, V Muscarello, G Bindolino, ... 70th International Annual Forum American Helicopter Society (AHS), 2381-2394, 2014 | 7 | 2014 |
Evaluation of rotorcraft aeroelastic stability using robust analysis G Quaranta, A Tamer, V Muscarello, P Masarati, M Gennaretti, J Serafini, ... | 7 | 2012 |
Biodynamic modeling techniques for rotorcraft comfort evaluation A Tamer, A Zanoni, V Muscarello, A Cocco, G Quaranta, P Masarati Aerotecnica Missili & Spazio 98 (2), 147-158, 2019 | 6 | 2019 |
Investigation of adverse aeroelastic rotorcraft-pilot coupling using real-time simulation V Muscarello, P Masarati, G Quaranta, L Lu, M Jump, M Jones 69th International Annual Forum American Helicopter Society (AHS), 1389-1407, 2013 | 6 | 2013 |
Anatomy, modelling and prediction of aeroservoelastic rotorcraft-pilot-coupling. M Gennaretti, MM Collela, J Serafini, BD Vu, P Masarati, G Quaranta, ... | 5 | 2013 |
Evaluation of vibration reduction devices for helicopter ride quality improvement A Tamer, V Muscarello, P Masarati, G Quaranta Aerospace Science and Technology 95, 105456, 2019 | 4 | 2019 |
Mulitple input describing function for non-linear analysis of ground and air resonance V Muscarello, G Quaranta | 4 | 2011 |
The role of flight simulation in exposing rotorcraft pilot couplings M Jones, M Jump, L Lu, D Yilmaz, MD Pavel, P Masarati, G Quaranta, ... Proceedings of the 39th European Rotorcraft Forum, Moscow, Russia, 2013 | 3 | 2013 |
Aeroelastic rotorcraft–pilot couplings in tiltrotor aircraft V Muscarello, F Colombo, G Quaranta, P Masarati Journal of Guidance, Control, and Dynamics 42 (3), 524-537, 2019 | 2 | 2019 |