Year | Paper |
2021 | Development and Testing of Classical Low Speed Envelope Tiltrotor Flight Control Laws |
2018 | Spilling the Silverware - High Angle of Attack Testing on the Newest Range of Gulfstream Business Class Airplanes |
2017 | Using Open Source Flight Simulation Software to Evaluate the Flying Qualities of an Autonomous Aircraft Performing a Longitudinal Tracking Task |
2017 | Identification of Aerodynamic Model of a Turboprop Trainer for the IPEV Flight Test Simulator |
2016 | Handling Qualities Evaluations of Unmanned Aircraft Systems |
2016 | E-2D Aerial Refueling Auxiliary Stability Augmentation System - The "Poor Man's Fly-by-Wire” |
2015 | Test for Test Training - Spinning the DG-1000S |
2015 | Finding Commonality in the Uncommon, Encountering PIO in Flight Test |
2013 | Unmanned Aircraft and the Applicability of Military Flying Qualities Standards |
2013 | Stalling Transport Aircraft |
2013 | Spin Reproduction, Control System Testing, and Control Room Training Using X-Plane |
2013 | Identification of High Angle of Attack Aerodynamic Model using Flight Data from Spin Tests |
2012 | Static VMCA Demonstrations |
2012 | Simplified Flight Test Instrumentation for VMCA De termination |
2012 | Post-Stall Model Identification from Flight Test Data |
2011 | Handling Qualities Flight Testing of the Stratospheric Observatory for Infrared Astronomy (SOFIA) |
2011 | What the Hell is Pilot Gain? |
2010 | Loss of Control Testing of Light Aircraft and a Cost-Effective Approach to Flight Test |
2010 | Near-Real-Time Stability & Control Flight Test Analysis of RQ-4 Block 20 AND Block 40 Global Hawk Aircraft |
2010 | C-12 Parameter Identification Flight Test Results and Instrumentation Requirements |
2009 | Real-time aerodynamic model parameter identification |
2006 | Dynamic Minimum Control Airspeed Testing of the US Navy Model E-2C Plus Aircraft Equipped with the Hamilton Sundstrand NP2000 Propeller System using a Split Throttle Test Technique |
2006 | JAS 39 Gripen Wake Vortex Penetration Flt Testing |
2006 | Tail Dihedral and Static Stability |
2005 | Shipboard STOVL Control Law Manual Mode and Autoland Development |
2005 | Boundary-Avoidance Tracking: A New Pilot Tracking Model |
2005 | Stall Testing of the U.S. Navy Model E-2C Plus Aircraft Equipped with the Hamilton Sundstrand NP2000 Propeller System |
2005 | Designing, Building & Flight Testing a Sport Biplane |
2005 | Flight Testing of Eurofighter Aircraft in the Asymmetric GBU-10 Configuration |
2004 | Parameter Determination for a Raptor 50 V2 Helicopter Dynamics Model |
2003 | X-31 VECTOR - Taking ESTOL to the Ground |
2002 | Flying Qualities Integration of the ATFLIR on the F/A-18E/F |
2002 | Propeller Slipstream Effects on Lateral and Directional Controllability of Multi-Engined Aircraft |
2001 | Modeling Abrupt Wing Stall from Flight Test Data |
2001 | Research on the Stability and Control of Soaring Birds Using Radio Controlled Gliders |
2000 | Improving Unmanned Aerial Vehicle Handling Qualities by Compensating for Time Delay |
2000 | F-22 Initial High Angle-of-Attack Flight Test Results |
1999 | Enhanced High AOA Maneuverability and Spin Recovery for the Super Hornet |
1998 | B-2 Flight Control System Development Flight Test Lessons Learned |
1998 | Lessons Learned from the F/A-18E/F High AGA Flight Test Development Program |
1998 | The X-36 Tailless Fighter Agility Research Aircraft |
1997 | Rotary Wing Handling Qualities for the 21st Century |
1997 | Gripen High Angle of Attack Testing |
1996 | Comparison of the Control Anticipation Parameter and the Bandwidth Criterion During the Landing Task |
1995 | HQDT - A Method for Predicting Handling Qualities in High Performance Aircraft |
1995 | Techniques Used for the Evaluation of Handling Qualities and Pilot-In-the-Loop Oscillation Susceptibility During the Flight Test of the C-17A Aircraft |
1995 | Using Single Surface Excitation for X-31 System Identification at High AoA |
1995 | From MECS to PECS - Testing of the Saab 2000 Elevator Control Systems |
1994 | Preliminary Handling Qualities Assessment of the N 250 Aircraft Design by Employing Piloted Flight Simulation Technique |
1994 | X-31 Post-Stall Envelope Expansion and Tactical Utility Testing |
1994 | F-16 Multi-Axis Thrust Vectoring Flight Test Program Overview |
1994 | Flight Testing Large Lateral Asymmetries on Highly Augmented Fighter/Attack Aircraft |
1993 | F-16 Handling Qualities Evaluation with Asymmetric Air-to-Ground External Stores |
1993 | The X-31 Team: Conquering Post Stall |
1993 | F/A-18 Controls Released Departure Recovery Flight Test Evaluation |
1992 | V-22 Tiltrotor Development & Flight Characteristics |
1992 | Flying-Qualities Flight Test of a Half-Scale Unmanned Air Vehicle |
1992 | High Alpha Testing of the AM-X Aircraft - Lessons Learned |
1992 | Aeroelastic Pilot-Induced Oscillation |
1992 | Flight Test Research for Longitudinal Oscillation of the FT-7 Aircraft |
1991 | Development of High AOA Nose Down Control Margin Guidelines for Relaxed Static Stability Tactical Jet Aircraft |
1991 | AV-8B Flight Test Operations for the 100% Leading Edge Root Extension Program |
1991 | Agility Flight Test Results |
1991 | Single Engine Testing of the F- 14A - PLUS in the Power Approach Configuration |
1991 | Development of a Personal Computer-Based Approach to Aircraft Parameter Identification |
1991 | Flight Test Research for Longitudinal Oscillation of FT-7 Aircraft |
1990 | Flying Qualities Testing on the Modern Technology Airship |
1990 | Handling and Performance Considerations When Conducting Air-to-Air Refueling of Large Aircraft by the Probe and Drogue System |
1990 | Estimation of Flying Qualities Using a Least Squares Lower-Order Equivalent Systems Technique |
1990 | X-29 High Angle of Attack Flight Test Procedures, Results, and Lessons Learned |
1989 | AM-X High Incidence Trials, Development and Results |
1989 | Minimum Control Speed - A 'Thrustless' Approach |
1989 | Flight-Test-Derived Stability Derivatives for the Advanced Technology Tactical Transport |
1989 | Estimation of Aerodynamic and Mode Parameters of Aircraft's Open and Closed-Loop System |
1988 | F-16N Supersonic Adversary Aircraft Evaluation |
1988 | Numerical Modeling of Flight Dynamics and Flight Test Data Identification of a Jet Trainer Airplane |
1987 | Dynamic Stability and Handling Qualities Tests on a Highly Augmented, Statically Unstable Airplane |
1987 | Determination of Rotor Derivatives and Rotor Hub Force and Moment Derivatives from Flight Measurements with the RSRA Compound Helicopter |
1987 | Application of Complementary Parameter Identification Techniques to Flight Test Data of a Transport Aircraft |
1987 | Identification of the DLC-Flap System of the Research Aircraft ATTAS |
1987 | Flight Test of the Advanced Electromechanical Actuation System |
1986 | Aerobatic Testing of the BK-117 Helicopter |
1986 | Full Envelope Aerodynamic Modeling of the Harrier Aircraft |
1985 | Flight Tests and Preliminary Aerodynamic Parameter Extraction of an Externally Piloted Vehicle Aircraft Model |
1984 | Results of High Angle-of-Attack Testing of the F-1 5 with Conformal Fuel Tanks |
1983 | Fighter Aircraft Dynamic Performance |
1982 | F-14 High Angle of Attack Investigation with Asymmetric Thrust and External Stores |
1982 | Engineering Aspects of the F/A-18A High AOA/Spin Program |
1982 | An In-Flight Investigation of Pilot-Induced Oscillation Suppression Filters During the Fighter Approach and Landing Task |
1982 | An Investigation of the Effects of a Thrust Augmenting Ejector on the Performance and Handling Qualities of an Upper Surface Blown Research Aircraft |
1981 | Cessna T303 Crusader |
1978 | An Evaluation of Sidestick Force/Deflection Characteristics on Aircraft Handling Qualities |
1978 | Design Developments Leading to Improved Flying Qualities of Fly-Powered Aircraft |
1978 | Evaluation of Selected Class III Requirements of M IL-F-8785B-ASG, Flying Qualities of Piloted Airplanes |
1978 | The Evolution of the High-Angle-of-Attack Features of the F-16 Flight Control System |
1978 | Estimation of Longitudinal Aircraft Characteristics Using Parameter Identification Techniques |
1978 | Considerations in the Analysis of Flight Test Maneuvers |
1978 | AFFTC Parameter Identification Experience |
1977 | The PIO Problem: Theory and Implications to Flight Test |
1976 | Frequency Domain Analysis of Closed-Loop Handling Qualities Flight Test Data |
1976 | Numerical Methods for Extracting MIL-F-8785B-ASG Flying Qualities Parameters from Flight Test Data |
1976 | Spin Testing Using Multiple Phototheodolites |
1976 | F-5E Spin Susceptibility Test Program |
1976 | Dynamic Test Techniques: Concepts and Practices |
1976 | AIDES - A Parameter Identification Program |
1976 | A Computer System for Identifying Aircraft Characteristics from Flight Test Data |
1975 | Spin Testing the Viggen Aircraft |
1975 | High Angle of Attack Flight Tests of the F-15 |
1975 | YF-17 Stall/Post-Stall Testing |
1975 | Stall/Post-Stall/Spin Avoidance Tests of the YA-10 Aircraft |
1975 | Determination of Minimum Catapult Launch Speeds |
1975 | A Comparison of Several Parameter Identification Techniques Applied to Flight Data from a Navy T-2 Aircraft |
1974 | NASA Flight Research Center Scale F-15 Remotely Piloted Research Vehicle Program |
1974 | SAAB-SCANIA Developed Method for Obtaining Stability Derivatives from Flight Tests |
1973 | Air-To-Air Tracking Techniques to Evaluate Aircraft Handling Qualities |
1973 | Piloted Power Approach Simulation |
1973 | An Investigation of the Rolling Stability Derivatives of a T-Tail Fighter Configuration at High Angles-of-Attack |
1973 | Flight Test Applications and Analysis of Parameter Identification Techniques |
1971 | NF-8D Variable Stability Program |
1970 | A Method for Obtaining Airplane Frequency Response from the Transient Response of the Airplane to a Known Input |
1970 | Use of Digital Computer Simulation in Evaluating Stability Derivative Extraction Techniques |