Padfield, Gareth - University of Liverpool

个人简介

I joined the University of Liverpool in 1999 after a 25 - year career in Government Research (The Royal Aircraft Establishment, DERA) and Industry, with the remit to develop and lead Aerospace Engineering research and teaching. My previous employment taught me many things about research and management but I am often reminded that committment to quality, integrity and passion are for me, the most important attributes. My passion for things Aerospace drives my committment, and has been with me from an early age. I held the post of Head of the School of Engineering from 2004-2010 and launched the University's Virtual Engineering Centre in 2009. Since retiring in 2011, I have continued to work with the Flight Science research group and in 2012 gave the Nikolsky lecture at the American Helicopter Society's annual forum in Fort Worth. In 2014 I published a new book - So you Want to be an Engineer; a guide to a wonderful, mysterious profession. The book draws on my experience as a practising engineer, and is aimed at students, educators and early career practitioners. I am available to present the essence of my guide to students in secondary and higher education. I also run a small technical consultancy, Flight Stability and Control, and have supported Industry and Governments on a wide range of projects over the last 15 years. Fellow of the Royal Academy of Engineering (Roayl Academy of Engineering 2008) key note speaker (Invitation to Speak, AHS 2007) Westland best paper prize (The RAeS 2006) best conference paper (Prize, Emerald Press 2005) Westland best paper Prize (Prize, The Royal Aeronautical Society 2004) Hodgson best paper prize (Prize, The Royal Aeronautical Society 2002) Best Human Factors paper (American Helicopter Society 2001) Bronze medal (Royal Aeronautical Society 1999)

研究领域

Flight Dynamics, Handling Qualities and Control Flight Simulation and Modelling Flight Safety and Human Factors

近期论文

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Optimising the roll-sway motion cues available from a short stroke hexapod motion platform. Rotorcraft Handling Qualities Engineering: Managing the Tension between Safety and Performance 32nd Alexander A. Nikolsky Honorary Lecture Simulating the Environment at the Aircraft-Ship Dynamic Interface: Development & Application Tau Guidance in Boundary-Avoidance Tracking - New Perspectives on Pilot-Induced Oscillations A Rating Scale for Subjective Assessment of Simulator Fidelity Fidelity enhancement of a rotorcraft simulation model through system identification Pilot Sensitivity to Flight Model Dynamics in Rotorcraft Simulation Virtual Engineering Centre - Examples of Virtual Prototyping and Multidisciplinary Design Optimization myCopter: Enabling Technologies For Personal Air Transport Systems - An Early Progress Report myCopter: Enabling Technologies for Personal Air Transport Systems "Progress in the development of unified fidelity metrics for rotorcraft flight simulators" Integrating Predicted and Perceived Fidelity for Flight Simulators Investigation of Rotorcraft-Pilot Couplings under Flight-Path Constraint below the Minimum-Power Speed Optical Tau in Boundary-Avoidance Tracking - A New Perspective on Pilot-Indiced Oscillations Physical motion but not auditory cues improve tracking performance in a simulated flight task Rotorcraft Simulation Renovation through System Identification Simulation of automatic helicopter deck landings using nature inspired flight control Tilt Rotor Pitch/Flight-Path Handling Qualities 'Acceptance testing of a rotorcraft flight simulator for research and teaching: the importance of unified metrics' 'Relationship between pilot workload and turbulence intensity for helicopter operations in harsh environments' 'Time-accurate ship airwake and unsteady aerodynamic loads modelling or maritime helicopter operations' Acceptance testing of a rotorcraft flight simulator for research and teaching: the importance of unified metric Rapid Prototyping and Validation of an Autogyro Simulation Model Simulated aerodynamic loading of an SH-60B helicopter in a ship's airwake 'Towards fully simulated ship-helicopter operating limits:The importance of ship airwake fidelity'