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Information on didactic, research and institutional assignments on this page are certified by the University; more information, prepared by the professor, are available on the personal web page and in the curriculum vitae indicated on this webpage.
Information on professor
ProfessorMasarati Pierangelo
QualificationFull professor full time
Belonging DepartmentDipartimento di Scienze e Tecnologie Aerospaziali
Scientific-Disciplinary SectorING-IND/04 - Aerospace Structures And Design
Curriculum VitaeDownload CV (114.8Kb - 04/05/2020)
OrcIDhttps://orcid.org/0000-0002-9347-7654

Contacts
Professor's office hours
DepartmentFloorOfficeDayTimetableTelephoneFaxNotes
Ingegneria Aerospaziale, Milano Bovisa, Edificio --41MondayFrom 14:30
To 16:30
(+39.02.2399).8309--Reception by appointment, arranged by telephone or email
E-mailpierangelo.masarati@polimi.it
Professor's personal websitehttps://home.aero.polimi.it/masarati/

Data source: RE.PUBLIC@POLIMI - Research Publications at Politecnico di Milano

List of publications and reserach products for the year 2021 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Journal Articles
On Task Dependence of Helicopter Pilot Biodynamic Feedthrough and Neuromuscular Admittance: An Experimental and Numerical Study (Show >>)


List of publications and reserach products for the year 2020 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Conference proceedings
A Novel Single-Step Unconditionally Stable Numerical Integration Scheme with Tunable Algorithmic Dissipation (Show >>)
A Virtual Reality Approach to Piloted Flight Simulation (Show >>)
Compliant Interface in Component Mode Synthesis (Show >>)
Design and Evaluation of a Constraint-Based Head-Up Display for Helicopter Obstacle Avoidance During Forward Flight (Show >>)
Effects of Flight Controls and Cockpit Layout Design in Rotorcraft-Pilot Couplings: a Computational Approach (Show >>)
Helicopter Pilot Biomechanics by Multibody Analysis (Show >>)
Smooth/Non-Smooth Multibody Co-Simulation of a Particle Damper (Show >>)
Uncertainty Quantification of Tiltrotor Whirl Flutter Aeroelastic Stability from Multibody Analysis (Show >>)
Journal Articles
A tight coupling scheme for smooth/non-smooth multibody co-simulation of a particle damper (Show >>)
Active isotropic compliance in redundant manipulators (Show >>)
Cabin Layout Optimization for Vibration Hazard Reduction in Helicopter Emergency Medical Service (Show >>)
Improved second-order unconditionally stable schemes of linear multi-step and equivalent single-step integration methods (Show >>)
Multibody dynamics analysis of the human upper body for rotorcraft–pilot interaction (Show >>)
On the optimization of n-sub-step composite time integration methods (Show >>)
Pilot in the Loop Simulation of Helicopter-Ship Operations Using Virtual Reality (Show >>)
State and force estimation on a rotating helicopter blade through a kalman-based approach (Show >>)


List of publications and reserach products for the year 2019 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Conference proceedings
Analysis of Rotorcraft Pilot Couplings from the Flight Control System Modes Perspective (Show >>)
Augmented Rotorcraft Conceptual Design Driven by Handling Qualities Requirements (Show >>)
Development of a Virtual Reality Real Time Helicopter Flight Simulator (Show >>)
Drivetrain Modeling Effects on Tiltrotor Aeroelastic Analysis (Show >>)
Flight Simulator Testing to Enhance Comprehension and Modeling of Rotorcraft Pilot Couplings (Show >>)
Flight Simulator Testing to Enhance Comprehension and Modeling of Rotorcraft Pilot Couplings (Show >>)
Generalized Measure of Vibration Exposure for Helicopter Pilots (Show >>)
Mathematical Modeling and Active Control of Smart Rotor Blade with Piezo-Composite Materials (Show >>)
Pilot Model Development and Human Manual Control Considerations for Helicopter Hover Displays (Show >>)
Rotorcraft-Pilot Coupling: a Multidisciplinary Point of View (Show >>)
Simulation and analysis of the influence of the support structure on a wind turbine gear set (Show >>)
Visual Performance Evaluation Of Helicopter Pilots In Vibrating Cockpit (Show >>)
Journal Articles
Active aeroelastic control of aircraft wings with piezo-composite (Show >>)
Aeroelastic Rotorcraft–Pilot Couplings in Tiltrotor Aircraft (Show >>)
Biodynamic Modeling Techniques for Rotorcraft Comfort Evaluation (Show >>)
Evaluation of vibration reduction devices for helicopter ride quality improvement (Show >>)
In-flight health monitoring of helicopter blades via differential analysis (Show >>)
Optimal Control of Pretwisted Rotating Thin-Walled Beams via Piezoelectrically Induced Couplings (Show >>)
Sensitivity of Lyapunov Exponents in Design Optimization of Nonlinear Dampers (Show >>)


List of publications and reserach products for the year 2018 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Abstract in Atti di convegno
Vortical Flow Airfoil Dynamics in Lie Group Setting: Geometric Reduction and Numerical Analysis (Show >>)
Patents
HELICOPTER KIT (Show >>)
Helicopter Kit (Show >>)
Helicopter Kit (Show >>)
Conference proceedings
A Comprehensive Aeroservoelastic Approach to Detect and Prevent Rotorcraft-Pilot Coupling Phenomena in Tiltrotors (Show >>)
A Handling Qualities Oriented Approach to Rotorcraft Conceptual Design (Show >>)
A Rotorcraft Conceptual Design Tool for Handling Qualities Evaluation (Show >>)
Assessment of the Feasibility of an Extended Range Helicopter Operational Standard for Offshore Flights (Show >>)
Autonomous Untethered Flight of Multibody Dynamics Rotorcraft With Cycloidal Rotors (Show >>)
FRAME-Sim: A Free-Software, Multibody-Based, Pilot in the Loop Rotorcraft Flight Simulator (Show >>)
Human Biodynamic Models for Rotorcraft Comfort Assessment (Show >>)
Rotorcraft-Pilot Couplings: Analysis and Detection in a Safety Enhancement Framework (Show >>)
Vibration Rating of Medical Helicopters (Show >>)
Journal Articles
Aeroelastic Analysis of a Cycloidal Rotor Under Various Operating Conditions (Show >>)
Ice Accretion Effects on Helicopter Rotor Performance, via Multibody and CFD Approaches (Show >>)
Instability Mechanism of Roll/Lateral Biodynamic Rotorcraft–Pilot Couplings (Show >>)
Rotor blade shape reconstruction from strain measurements (Show >>)


List of publications and reserach products for the year 2017 (Show all details | Hide all details)
Type Title of the Publicaiton/Product
Abstract in Atti di convegno
Benchmark Problems for the Linearization of Multibody Dynamics (Show >>)
Patents
Rotor For A Hover-Capable Aircraft And Method For Containment Of Vibrations Transmitted To The Mast Of A Rotor Of A Hover-Capable Aircraft (Show >>)
Conference proceedings
A Virtual Environment for Rotorcraft Vibration Analysis (Show >>)
Benchmarking of Linearization Methods for Multibody System Dynamics (Show >>)
Dynamic Analysis of a 3D Printer Based on the Delta Mechanism (Show >>)
Novel Approach to Interaction Between Engine-Drive Train System and Deformable Rotorcraft Airframes (Show >>)
Optimal Control of Pretwisted Adaptive Rotating Blades Modeled as Anisotropic Thin-Walled Beams with Piezo-Composite (Show >>)
Quantitative Aeroelastic Stability Evaluation of Control Surfaces with Structural Nonlinearities (Show >>)
Rotor State Evaluation and Structural Health Monitoring Through Strain Sensors (Show >>)
Shape Sensing and Structural Health Monitoring of Rotor Blades from Strain Analysis (Show >>)
Journal Articles
Aeroelastic Stability Estimation of Control Surfaces with Freeplay Nonlinearity (Show >>)
Assessment of Linearization Approaches for Multibody Dynamics Formulations (Show >>)
Membrane Shape and Load Reconstruction from Measurements Using Inverse Finite Element Analysis (Show >>)
Modeling and control for rotating pretwisted thin-walled beams with piezo-composite (Show >>)
Modeling effects of membrane tension on dynamic stall for thin membrane wings (Show >>)
N-body gravitational and contact dynamics for asteroid aggregation (Show >>)
Parametric Analysis of a Large-Scale Cycloidal Rotor in Hovering Conditions (Show >>)
Robust Stability Analysis of Adverse Aeroelastic Roll/Lateral Rotorcraft–Pilot Couplings (Show >>)
Velocity feedback damping of piezo-actuated wings (Show >>)
manifesti v. 3.4.7 / 3.4.7
Area Servizi ICT
20/01/2021