Publications
Selected publications
- The potential impact of adverse aircraft-pilot couplings on the safety of tilt-rotor operations (Journal article - 2022)
- Rotorcraft Handling Qualities Engineering: Managing the Tension between Safety and Performance <i>32nd Alexander A. Nikolsky Honorary Lecture</i> (Journal article - 2013)
- Simulating the Environment at the Aircraft-Ship Dynamic Interface: Development & Application (Journal article - 2012)
- Tau Guidance in Boundary-Avoidance Tracking - New Perspectives on Pilot-Induced Oscillations (Journal article - 2012)
- Optimising the roll-sway motion cues available from a short stroke hexapod motion platform (Journal article - 2015)
- Optimising the yaw motion cues available from a short stroke hexapod motion platform (Journal article - 2015)
- Fidelity enhancement of a rotorcraft simulation model through system identification (Journal article - 2011)
- Investigation of Rotorcraft-Pilot Couplings under Flight-Path Constraint below the Minimum-Power Speed (Journal article - 2010)
- Simulation of automatic helicopter deck landings using nature inspired flight control (Journal article - 2010)
- Capturing requirements for tiltrotor handling qualities – case studies in virtual engineering (Journal article - 2008)
2022
The potential impact of adverse aircraft-pilot couplings on the safety of tilt-rotor operations
Padfield, G. D., & Lu, L. (2022). The potential impact of adverse aircraft-pilot couplings on the safety of tilt-rotor operations. AERONAUTICAL JOURNAL, 126(1304), 1617-1647. doi:10.1017/aer.2022.20
2015
Optimising the roll-sway motion cues available from a short stroke hexapod motion platform
Hodge, S., Perfect, P., Padfield, G., & White, M. (2015). Optimising the roll-sway motion cues available from a short stroke hexapod motion platform. The Aeronautical Journal, 119(1121), 23-44.
Optimising the yaw motion cues available from a short stroke hexapod motion platform
Hodge, S., Perfect, P., Padfield, G., & White, M. (2015). Optimising the yaw motion cues available from a short stroke hexapod motion platform. The Aeronautical Journal, 119(1121), 1-21.
Optimising the yaw motion cues available from a short stroke hexapod motion platform
Hodge, S. J., Perfect, P., Padfield, G. D., & White, M. D. (2015). Optimising the yaw motion cues available from a short stroke hexapod motion platform. In AERONAUTICAL JOURNAL Vol. 119 (pp. 1-21). Retrieved from https://www.webofscience.com/
2013
Rotorcraft Handling Qualities Engineering: Managing the Tension between Safety and Performance <i>32nd Alexander A. Nikolsky Honorary Lecture</i>
Padfield, G. D. (2013). Rotorcraft Handling Qualities Engineering: Managing the Tension between Safety and Performance <i>32nd Alexander A. Nikolsky Honorary Lecture</i>. Journal of the American Helicopter Society, 58(1), 1-27. doi:10.4050/jahs.58.011001
2012
Simulating the Environment at the Aircraft-Ship Dynamic Interface: Development & Application
Padfield, G. D. (2012). Simulating the Environment at the Aircraft-Ship Dynamic Interface: Development & Application. The Aeronautical Journal of the RAeS.
Tau Guidance in Boundary-Avoidance Tracking - New Perspectives on Pilot-Induced Oscillations
Padfield, G. D., Lu, L., & Jump, M. (2012). Tau Guidance in Boundary-Avoidance Tracking - New Perspectives on Pilot-Induced Oscillations. Journal of Guidance, Control, and Dynamics, 35(1), 80-92. doi:10.2514/1.54065
2011
A Rating Scale for Subjective Assessment of Simulator Fidelity
Perfect, P. S., Timson, E., White, M. D., Padfield, G. D., Erdos, R., Gubbels, A. W., & Berryman, A. C. (2011). A Rating Scale for Subjective Assessment of Simulator Fidelity. In European Rotorcraft Forum (pp. pp1-pp12). Gallarate: European Rotorcraft Forum.
Fidelity enhancement of a rotorcraft simulation model through system identification
Lu, L., Padfield, G. D., White, M., & Perfect, P. (2011). Fidelity enhancement of a rotorcraft simulation model through system identification. AERONAUTICAL JOURNAL, 115(1170), 453-470. doi:10.1017/S0001924000006102
Pilot Sensitivity to Flight Model Dynamics in Rotorcraft Simulation
Timson, E., Perfect, P. S., White, M. D., Padfield, G. D., Erdos, R., & Gubbels, A. W. (2011). Pilot Sensitivity to Flight Model Dynamics in Rotorcraft Simulation. In European Rotorcraft Forum (pp. pp1-pp14). Gallarate: European Rotorcraft Forum.
Virtual Engineering Centre - Examples of Virtual Prototyping and Multidisciplinary Design Optimization
Cooper, J. E., & al, E. (2011). Virtual Engineering Centre - Examples of Virtual Prototyping and Multidisciplinary Design Optimization. In Virtual Prototyping of Affordable Military Vehicles Using Advanced MDO (pp. 1-28). Sofia, Bulgaria: NATO.
myCopter: Enabling Technologies For Personal Air Transport Systems - An Early Progress Report
Jump, M., & al., E. (2011). myCopter: Enabling Technologies For Personal Air Transport Systems - An Early Progress Report. In 37th European Rotorcraft Forum (pp. 1-12). Gallarate: ERF.
myCopter: Enabling Technologies for Personal Air Transport Systems
Jump, M., & al., E. (2011). myCopter: Enabling Technologies for Personal Air Transport Systems. In The Future Rotorcraft - Enabling Capability Through the Application of Technology (pp. 1-15). London: The Royal Aeronautical Society.
2010
"Progress in the development of unified fidelity metrics for rotorcraft flight simulators",
White, M. D., Perfect, P., Padfield, G. D., Gubbels, A. W., & Berryman, A. C. (2010). "Progress in the development of unified fidelity metrics for rotorcraft flight simulators",. In 66th Annual Forum of the American Helicopter Society (pp. 1-20). Phoenix: AHS.
Integrating Predicted and Perceived Fidelity for Flight Simulators
Perfect, P., White, M. D., & Padfield, G. D. (2010). Integrating Predicted and Perceived Fidelity for Flight Simulators. In 36th European Rotorcraft Forum (pp. 1-20). Paris: CEAS.
Investigation of Rotorcraft-Pilot Couplings under Flight-Path Constraint below the Minimum-Power Speed
Lu, L., Padfield, G. D., & Jump, M. (2010). Investigation of Rotorcraft-Pilot Couplings under Flight-Path Constraint below the Minimum-Power Speed. The Aeronautical Journal, 114(1155).
Optical Tau in Boundary-Avoidance Tracking - A New Perspective on Pilot-Indiced Oscillations
Lu, L., Padfield, G., & Jump, M. (2010). Optical Tau in Boundary-Avoidance Tracking - A New Perspective on Pilot-Indiced Oscillations. In 36th European Rotorcraft Forum (pp. pp). Paris, France: ERF.
Optical tau in boundary-avoidance tracking - a new perspective on pilot-induced oscillations
Lu, L., Padfield, G. D., & Jump, M. (2010). Optical tau in boundary-avoidance tracking - a new perspective on pilot-induced oscillations. In 36th European Rotorcraft Forum (pp. 1-18). Paris: RAes.
Physical motion but not auditory cues improve tracking performance in a simulated flight task
Meyer, G. F., Furber, H., White, M. D., Perfect, P., & Padfield, G. (2010). Physical motion but not auditory cues improve tracking performance in a simulated flight task. 11th International Multisensory Research Forum, 0, 213. Retrieved from http://imrf.mcmaster.ca/IMRF/ocs2/index.php/imrf/2010/presenter/submission/213
Rotorcraft Simulation Renovation through System Identification
Lu, L., & Padfield, G. D. (2010). Rotorcraft Simulation Renovation through System Identification. In 36th European Rotorcraft Forum, (pp. 1-20). Paris: CEAS.
Simulation of automatic helicopter deck landings using nature inspired flight control
Voskuijl, M., Padfield, G. D., Walker, D. J., Manimala, B. J., & Gubbels, A. W. (2010). Simulation of automatic helicopter deck landings using nature inspired flight control. The Aeronautical Journal, 114(1151), 25-34. doi:10.1017/s000192400000350x
Tilt Rotor Pitch/Flight-Path Handling Qualities
Cameron, N., & Padfield, G. D. (2010). Tilt Rotor Pitch/Flight-Path Handling Qualities. Journal of the American Helicopter Society, 55(4), 40-60.
2009
Relationship between pilot workload and turbulence intensity for helicopter operations in harsh environments
Matayoshi, N., Forrest, J. S., Hodge, S. J., Padfield, G. D., & Owen, I. (2009). Relationship between pilot workload and turbulence intensity for helicopter operations in harsh environments. In Annual Forum Proceedings AHS International Vol. 2 (pp. 1595-1603).
Time-Accurate Ship Airwake and Unsteady Aerodynamic Loads Modeling for Maritime Helicopter Simulation
Hodge, S. J., Zan, S. J., Roper, D. M., Padfield, G. D., & Owen, I. (2009). Time-Accurate Ship Airwake and Unsteady Aerodynamic Loads Modeling for Maritime Helicopter Simulation. JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 54(2). doi:10.4050/JAHS.54.022005
'Acceptance testing of a rotorcraft flight simulator for research and teaching: the importance of unified metrics'
White, M., Perfect, P., Padfield, G. D., & Gubbels, A. (2009). 'Acceptance testing of a rotorcraft flight simulator for research and teaching: the importance of unified metrics'. In 35th European Rotorcraft Forum (pp. 1-20). Hamburg: CEAS.
Acceptance testing of a rotorcraft flight simulator for research and teaching: the importance of unified metric
White, M., Perfect, P., Padfield, G. D., & Gubbels, A. (2009). Acceptance testing of a rotorcraft flight simulator for research and teaching: the importance of unified metric. In CEAS 2009 (pp. 1-20). Manchester: CEAS.
Rapid Prototyping and Validation of an Autogyro Simulation Model
Jump, M., Kendrick, S., Perfect, P., Padfield, G. D., & Ridgway, G. R. (2009). Rapid Prototyping and Validation of an Autogyro Simulation Model. In CEAS 2009 European Air and Space Conference (pp. 1-17). Manchester: CEAS.
Simulated aerodynamic loading of an SH-60B helicopter in a ship's airwake
Kaaria, C., Forrest, J., Padfield, G. D., & Owen, I. (2009). Simulated aerodynamic loading of an SH-60B helicopter in a ship's airwake. In 35th European Rotorcraft Forum (pp. 1-20). Hamburg: CEAS.
2008
Towards fully simulated ship-helicopter operating limits: The importance of ship airwake fidelity
Forrest, J. S., Hodge, S. J., Owen, I., & Padfield, G. D. (2008). Towards fully simulated ship-helicopter operating limits: The importance of ship airwake fidelity. In Annual Forum Proceedings AHS International Vol. 1 (pp. 339-351).
Capturing requirements for tiltrotor handling qualities – case studies in virtual engineering
Padfield, G. D. (2008). Capturing requirements for tiltrotor handling qualities – case studies in virtual engineering. The Aeronautical Journal, 112(1134), 433-448. doi:10.1017/s0001924000002402
Wake vortex encounter severity for rotorcraft in final approach
Lawrence, B., & Padfield, G. D. (2008). Wake vortex encounter severity for rotorcraft in final approach. Aerospace Science and Technology, 12(5), 385-397. doi:10.1016/j.ast.2007.09.006
Vehicle Guidance System
Jump, M., Padfield, G. D., & Lee, D. N. (2008). Vehicle Guidance System.
Determining Fidelity Standards for Maritime Rotorcraft Simulation
Hodge, S. J., Forrest, J. S., Padfield, G. D., & White, M. D. (2008). Determining Fidelity Standards for Maritime Rotorcraft Simulation. In Maritime Operations of Rotorcraft. London: The Royal Aeronautical Society.
Handling Qualities through a virtual engineering lens
Padfield, G. D. (2008). Handling Qualities through a virtual engineering lens. In Rotorcraft Handling Qualities (pp. 1-20). Liverpool, England: RAeS.
Investigation of Aircraft-Pilot Couplings under Flight-Path Constraint below the Minimum-Power Speed
Padfield, G. D. (2008). Investigation of Aircraft-Pilot Couplings under Flight-Path Constraint below the Minimum-Power Speed. In Rotorcraft Handling Qualities (pp. 1-20). Liverpool, England: RAeS.
The strongly controlled helicopter
Padfield, G. D. (2008). The strongly controlled helicopter. In 34th European Rotorcraft Forum (pp. 1-20). Liverpool, England: RAeS.
Towards fully simulated ship-helicopter operating limits ; the importance of ship airwake fidelity
Padfield, G. D. (2008). Towards fully simulated ship-helicopter operating limits ; the importance of ship airwake fidelity. In 64th annual forum of the American Helicopter Society (pp. 2-20). Montreal, Canada: AHS.
preparing for the 4-dimensional world of the professional engineer
Padfield, G. D. (2008). preparing for the 4-dimensional world of the professional engineer. Aerospace Professional, 10-13.
understanding the peculiarities of rotorcraft-pilot couplings
Padfield, G. D. (2008). understanding the peculiarities of rotorcraft-pilot couplings. In 64th annual forum of the American Helicopter Society (pp. 1-20). Montreal, Canada: AHS.
2007
Development of a Nature-Inspired Flare Command Algorithm
Jump, M., & Padfield, G. (2007). Development of a Nature-Inspired Flare Command Algorithm. In AIAA Guidance, Navigation and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2007-6769
How Long Do Pilots Look Forward? Prospective Visual Guidance in Terrain-Hugging Flight
Padfield, G. D., Clark, G., & Taghizad, A. (2007). How Long Do Pilots Look Forward? Prospective Visual Guidance in Terrain-Hugging Flight. Journal of the American Helicopter Society, 52(2), 134-145. doi:10.4050/jahs.52.134
Rotorcraft simulation modelling and validation for control law design
Manimala, B. J., Walker, D. J., Padfield, G. D., Voskuijl, M., & Gubbels, A. W. (2007). Rotorcraft simulation modelling and validation for control law design. The Aeronautical Journal, 111(1116), 77-88. doi:10.1017/s0001924000001780
Capturing Requirements for Tilt Rotor Handling Qualities; case studies in virtual engineering
Padfield, G. D. (2007). Capturing Requirements for Tilt Rotor Handling Qualities; case studies in virtual engineering. In AHS Conference on Multi-Disciplinary Rotrocraft Technology (pp. 1-15). Soeul: AHS.
Helicopter Flight Dynamics
Padfield, G. D. (2007). Helicopter Flight Dynamics. Oxford: Blackwell Science.
Helicopter Flight Dynamics
Padfield, G. D. (2007). Helicopter Flight Dynamics. Wiley. doi:10.1002/9780470691847
Tilt Rotor Pitch/Flight-Path Handling Qualities
Cameron, N., & Padfield, G. D. (2007). Tilt Rotor Pitch/Flight-Path Handling Qualities. In Annual Forum of the American Helicopter Society (pp. 1-20). Virginia Beach: AHS.
UNIFIED TILT ROTOR HANDLING QUALITIES; FEASIBLE OR IMPRACTICABLE ? part 1 - setting the challenge
Cameron, N., Perfect, P., Padfield, G. D., & Walker, D. (2007). UNIFIED TILT ROTOR HANDLING QUALITIES; FEASIBLE OR IMPRACTICABLE ? part 1 - setting the challenge. In 33rd European Rotorcraft Forum (pp. 1-15). Kazan: ERF.
UNIFIED TILT ROTOR HANDLING QUALITIES; feasible or impractiable? Part 2 control concepts
Perfect, P., Padfield, G. D., Cameron, N., & Walker, D. (2007). UNIFIED TILT ROTOR HANDLING QUALITIES; feasible or impractiable? Part 2 control concepts. In 33rd European Rotorcraft Forum (pp. 1-15). Kazan: ERF.
2006
Flexible Uses of Simulation Tools in an Academic Environment
Lawrence, B., Padfield, G., & Perfect, P. (2006). Flexible Uses of Simulation Tools in an Academic Environment. In AIAA Modeling and Simulation Technologies Conference and Exhibit. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2006-6808
Flight Handling Qualities; a pbl module for aerospace engineering students
Padfield, G. D. (2006). Flight Handling Qualities; a pbl module for aerospace engineering students. The Aeronautical Journal, 110(1104), 73-84.
Flight handling qualities of the Wright Flyer III
Lawrence, B., & Padfield, G. D. (2006). Flight handling qualities of the Wright Flyer III. AIAA J. of Aircraft, 43(5), 1307-1316.
Helicopter-ship dynamic interface: high-fidelity simulation at low-cost,
Hodge, S., Padfield, G., & Southworth, M. (2006). Helicopter-ship dynamic interface: high-fidelity simulation at low-cost,. In Cutting Costs in Flight Simulation : Balancing Quality and Capability (pp. 24-40). London: RAeS.
Investigation of the Flare Maneuver Using Optical Tau
Jump, M., & Padfield, G. D. (2006). Investigation of the Flare Maneuver Using Optical Tau. Journal of Guidance, Control, and Dynamics, 29(5), 1189-1200. doi:10.2514/1.20012
Load Alleviation for Tilt Rotor Aircraft in Airplane Mode, Journal of Aircraft
Manimala, B., Padfield, G. D., & Walker, D. J. (2006). Load Alleviation for Tilt Rotor Aircraft in Airplane Mode, Journal of Aircraft. Journal of Aircraft, 43(1), 147-156.
Load Alleviation for a Tilt-Rotor Aircraft in Airplane Mode
Manimala, B., Padfield, G. D., & Walker, D. (2006). Load Alleviation for a Tilt-Rotor Aircraft in Airplane Mode. Journal of Aircraft, 43(1), 147-156. doi:10.2514/1.13565
Progress in Civil Tilt-Rotor Handling Qualities
Padfield, G. D., Brookes, V., & Meyer, M. A. (2006). Progress in Civil Tilt-Rotor Handling Qualities. Journal of the American Helicopter Society, 51(1), 80. doi:10.4050/1.3092880
Progress in the development of guidance strategies for the landing flare manoeuvre using tau‐based parameters
Jump, M., & Padfield, G. D. (2006). Progress in the development of guidance strategies for the landing flare manoeuvre using tau‐based parameters. Aircraft Engineering and Aerospace Technology, 78(1), 4-12. doi:10.1108/17488840610639618
ROTORCRAFT WAKE VORTEX ENCOUNTERS: a flight mechanics perspective
Lawrence, B., Padfield, G., & Taghizard, A. (2006). ROTORCRAFT WAKE VORTEX ENCOUNTERS: a flight mechanics perspective. In 32nd European Rotorcraft Forum (pp. 200-2020). Maastricht: ERF.
The extension of ADS-33 metrics for agility enhancement and structural load alleviation
Pavel, M., & Padfield, G. D. (2006). The extension of ADS-33 metrics for agility enhancement and structural load alleviation. Journal of the Americal Helicopter Society, 51(4), 319-330.
2005
Tau Flare or not Tau Flare: That is the question: Developing guidelines for an approach and landing sky guide
Jump, M., & Padfield, G. D. (2005). Tau Flare or not Tau Flare: That is the question: Developing guidelines for an approach and landing sky guide. In Collection of Technical Papers AIAA Guidance Navigation and Control Conference Vol. 7 (pp. 5551-5568).
Tau Flare or not Tau Flare: that is the question: Developing Guidelines for an Approach and Landing Sky Guide
Jump, M., & Padfield, G. (2005). Tau Flare or not Tau Flare: that is the question: Developing Guidelines for an Approach and Landing Sky Guide. In AIAA Guidance, Navigation, and Control Conference and Exhibit. American Institute of Aeronautics and Astronautics. doi:10.2514/6.2005-6404
The birth of the practical aeroplane: An appraisal of the Wright brothers’ achievements in 1905
Padfield, G. D., & Lawrence, B. (2005). The birth of the practical aeroplane: An appraisal of the Wright brothers’ achievements in 1905. The Aeronautical Journal, 109(1098), 421-437. doi:10.1017/s000192400000083x
Measuring simulation fidelity through an adaptive pilot model
Padfield, G., & White, M. (2005). Measuring simulation fidelity through an adaptive pilot model. AEROSPACE SCIENCE AND TECHNOLOGY, 9(5), 400-408. doi:10.1016/j.ast.2005.03.004
'Progress in the development of guidance strategies for the landing flare manoeuvre using tau-based parameters
Jump, M., & Padfield, G. D. (2005). 'Progress in the development of guidance strategies for the landing flare manoeuvre using tau-based parameters. In 1st International Conference on Innovation & Integration in Aerospace Sciences (pp. 0). Belfast: CEIAT.
First Steps in the Development of Handling Qualities Criteria for a Civil Tilt Rotor
Meyer, M. A., & Padfield, G. D. (2005). First Steps in the Development of Handling Qualities Criteria for a Civil Tilt Rotor. Journal of the American Helicopter Society, 50(1), 33-45. doi:10.4050/1.3092841
Flight Handling Qualities of the Wright Flyer III
Lawrence, B., & Padfield, G. D. (2005). Flight Handling Qualities of the Wright Flyer III. In Unknown Conference Vol. 43 (pp. 1307-1316). Reno.
Flight handling qualities; a problem based learning module for final year aerospace engineering students
Padfield, G. D. (2005). Flight handling qualities; a problem based learning module for final year aerospace engineering students. Kingston, Ontario.
Handling Qualities Analysis of the Wright Brothers' 1902 Glider
Lawrence, B., & Padfield, G. D. (2005). Handling Qualities Analysis of the Wright Brothers' 1902 Glider. Journal of Aircraft, 42(1), 224-236. doi:10.2514/1.6091
How long do pilots look forward? Prospective visual guidance in terrain hugging flight
Padfield, G. D., Clark, G., & Taghizard, A. (2005). How long do pilots look forward? Prospective visual guidance in terrain hugging flight. In Unknown Conference Vol. 52 (pp. 134-145). Florence, Italy.
Progress in the Development of Guidance Strategies for the Landing Flare Manoeuvre Using Tau-based Parameters
Jump, M., & Padfield, G. D. (2005). Progress in the Development of Guidance Strategies for the Landing Flare Manoeuvre Using Tau-based Parameters. Belfast (best paper prize).
Simulation fidelity of real-time helicopter simulation models
Padfield, G. D. (2005). Simulation fidelity of real-time helicopter simulation models. Grapevine, Tx.
Synthesis and analysis of a multi-objective controller for tilt-rotor structural load alleviation
Manimala, B., Padfield, G. D., Walker, D., & Childs, S. (2005). Synthesis and analysis of a multi-objective controller for tilt-rotor structural load alleviation. Belfast.
The use of CFD and piloted flight simulation for measuring workload at the helicopter-ship dynamic interface
Roper, D., Hodge, S., Padfield, G. D., & Owen, I. (2005). The use of CFD and piloted flight simulation for measuring workload at the helicopter-ship dynamic interface. Grapevine, Tx.
Vortex wake encounter severity for rotorcraft in approach and landing
Lawrence, B., & Padfield, G. D. (2005). Vortex wake encounter severity for rotorcraft in approach and landing. Florence, Italy.
2004
A Severity Analysis for Rotorcraft Encounters with Vortex Wakes
Padfield, G. D., Manimala, B., & Turner, G. P. (2004). A Severity Analysis for Rotorcraft Encounters with Vortex Wakes. Journal of the American Helicopter Society, 49(4), 445-456. doi:10.4050/jahs.49.445
Flight simulation in academia - Progress with HELIFLIGHT at the University of Liverpool
White, M. D., & Padfield, G. D. (2004). Flight simulation in academia - Progress with HELIFLIGHT at the University of Liverpool. London, UK.
Handling qualities degradation in tilt rotor aircraft following flight control system failures
Cameron, N., & Padfield, G. D. (2004). Handling qualities degradation in tilt rotor aircraft following flight control system failures. Marseilles, France.
Load Alleviation in Tilt Rotor Aircraft through Active Control; Modelling and Control Concepts
Manimala, B., Padfield, G. D., Walker, D., Naddei, M., Verde, L., Ciniglio, U., . . . Sandri, F. (2004). Load Alleviation in Tilt Rotor Aircraft through Active Control; Modelling and Control Concepts. The Aeronautical Journal of the Royal Aeronautical Society, 108(1082), 169-185.
Progress with the adaptive pilot model in simulation fidelity
White, M. D., & Padfield, G. D. (2004). Progress with the adaptive pilot model in simulation fidelity. Baltimore, MD.
Validation criteria for helicopter real-time simulation models; Sketches from the work of GARTEUR AG-12
Padfield, G. D. (2004). Validation criteria for helicopter real-time simulation models; Sketches from the work of GARTEUR AG-12. Marseilles, France.
2003
The birth of flight control: An engineering analysis of the Wright brothers’ 1902 glider
Padfield, G. D., & Lawrence, B. (2003). The birth of flight control: An engineering analysis of the Wright brothers’ 1902 glider. The Aeronautical Journal, 107(1078), 697-718. doi:10.1017/s0001924000013464
'Flight Simulation in Academia: HELIFLIGHT in its First Year of Operation'
Padfield, G. D., & White, M. D. (2003). 'Flight Simulation in Academia: HELIFLIGHT in its First Year of Operation'. The Aeronautical Journal, 107(1075), 529-538.
Flight Simulation in Academia; HELIFLIGHT in its first year of operation
Padfield, G. D., & White, M. D. (2003). Flight Simulation in Academia; HELIFLIGHT in its first year of operation. The Aeronautical Journal of the Royal Aeronautical Society, 107(1075), 529-538.
Flight testing simulations of the Wright 1902 Glider and 1903 Flyer
Lawrence, B., & Padfield, G. D. (2003). Flight testing simulations of the Wright 1902 Glider and 1903 Flyer. Portsmouth, Va (received best paper award).
How do pilots know when to stop, turn or pull-up? Developing guidelines for the design of vision aids
Padfield, G. D., Lee, D., & Bradley, R. (2003). How do pilots know when to stop, turn or pull-up? Developing guidelines for the design of vision aids. J. American Helicopter Society, 48(2), 108-119.
Progress in civil tilt rotor handling qualities
Padfield, G. D., & Meyer, M. (2003). Progress in civil tilt rotor handling qualities. Friedrichstrafen.
Progress in the development of complementary handling and loading metrics for ADS-33 manoeuvres
Pavel, M., & Padfield, G. D. (2003). Progress in the development of complementary handling and loading metrics for ADS-33 manoeuvres. Phoenix, Az, USA.
2002
Encounters with Aircraft Vortex Wakes: The Impact on Helicopter Handling Qualities
Turner, G. P., Padfield, G. D., & Harris, M. (2002). Encounters with Aircraft Vortex Wakes: The Impact on Helicopter Handling Qualities. Journal of Aircraft, 39(5), 839-849. doi:10.2514/2.3004
Defining consistent ADS-33 metrics for agility enhancement and structural load alleviation
Pavel, M., & Padfield, G. D. (2002). Defining consistent ADS-33 metrics for agility enhancement and structural load alleviation. Montreal, USA.
2001
Helicopter encounters with aircraft vortex wakes
Padfield, G. D., & Turner, G. P. (2001). Helicopter encounters with aircraft vortex wakes. The Aeronautical Journal, 105(1043), 1-8. doi:10.1017/s0001924000095920