Subject: (08) Aircraft Stability And Control
Number of records: 246.
Sim, Alex G. (1997) A Correlation Between Flight-Determined Derivatives and Wind-Tunnel Data for the X-24B Research Aircraft. Technical Report NASA TM-113084, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Cox, Timothy H. (1989) A Design Procedure for the Handling Qualities Optimization of the X-29A Aircraft. Technical Report NASA TM-4142, Research Engineering, NASA Dryden Flight Research Center.
Roncoli, Ralph B. (1982) A Flight Test Maneuver Autopilot For a Highly Maneuverable Aircraft. Technical Report NASA TM-81372, Research Engineering, NASA Dryden Flight Research Center.
Berry, Donald T. (1986) A Flightpath Overshoot Flying Qualities Metric for the Landing Task. Technical Report NASA TM-86795, Research Engineering, NASA Dryden Flight Research Center.
Hanson, Curtis E. (2003) A Fuzzy Technique for Performing Lateral-Axis Formation Flight Navigation Using Wingtip Vortices. Technical Report NASA/TM-2003-212033, Research Engineering, NASA Dryden Flight Research Center.
Cotting, M. Christopher and Cox, Timothy H. (2005) A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. Technical Report NASA/TM-2005-212866, Research Engineering, NASA Dryden Flight Research Center.
Cotting, M. Christopher and Cox, Timothy H. (2005) A Generic Guidance and Control Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. Meeting Presentation AIAA-2005-0032, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Cotting, M. Christopher (2005) A Generic Inner-Loop Control Law Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. Technical Report NASA/TM-2005-212865, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Cotting, M. Christopher (2005) A Generic Inner-Loop Control Law Structure for Six-Degree-of-Freedom Conceptual Aircraft Design. Meeting Presentation AIAA-2005-0031, Research Engineering, NASA Dryden Flight Research Center.
Ryan III, George W. (1995) A Genetic Search Technique for Identification of Aircraft Departures. Technical Report NASA CR-4688, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and McNeill, Walter E. and Gilyard, Glenn B. and Maine, Trindel A. (1988) A Piloted Evaluation of an Oblique-Wing Research Aircraft Motion Simulation With Decoupling Control Laws. Technical Report NASA TP-2874, Research Engineering, NASA Dryden Flight Research Center.
Azzano, Christopher P. (1992) A Preliminary Look at an Optimal Multivariable Design for Propulsion-Only Flight Control of Jet-Transport Aircraft. Technical Report NASA CR-186014, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick C. (1997) A Presentation on Robust Flutter Margin Analysis and a Flutterometer. Technical Report NASA/TM-97-206220, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Conley, Joseph L. and Le, Jeanette and Burcham Jr., Frank W. (1991) A Simulation Evaluation of a Four-Engine Jet Transport Using Engine Thrust Modulation for Flightpath Control. Technical Report NASA TM-4324, Research Engineering, NASA Dryden Flight Research Center.
Cumming, Stephen B. and Diebler, Corey G. (2005) Active Aeroelastic Wing Aerodynamic Model Development and Validation for a Modified F/A-18A. Meeting Paper AIAA-2005-6312, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1984) Active Control Technology Experience With the Space Shuttle in the Landing Regime. Technical Report NASA TM-85910, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. (1993) Actuator and Aerodynamic Modeling for High-Angle-of-Attack Aeroservoelasticity. Technical Report NASA TM-4493, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Williams-Hayes, Peggy and Kaneshige, John T. and Stachowiak, Susan J. (2006) Adaptive Control Using Neural Network Augmentation for a Modified F-15 Aircraft. Conference Presentation WEA-1, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Alag, Gurbux S. and Gilyard, Glenn B. (1986) Aeroelastic Control of Oblique-Wing Aircraft. Technical Report NASA TM-86808, Research Engineering, NASA Dryden Flight Research Center.
Kukreja, Sunil L. (2007) Aeroelastic Model Structure Computation for Envelope Expansion. Technical Report NASA/TM-2007-214623, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. and Prazenica, Richard J. (2003) Aeroservoelastic Model Validation and Test Data Analysis of the F/A-18 Active Aeroelastic Wing. Technical Report NASA/TM-2003-212021, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. (1996) Aeroservoelastic Modeling and Validation of a Thrust-Vectoring F/A-18 Aircraft. Technical Report NASA TP-3647, Research Engineering, NASA Dryden Flight Research Center.
Pak, Chan-gi (2008) Aeroservoelastic Stability Analysis of the X-43A Stack. Technical Report NASA/TM-2008-214635, Research and Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. (2001) Aeroservoelastic Uncertainty Model Identification From Flight Data. Technical Report NASA/TM-2001-210397, Research Engineering, NASA Dryden Flight Research Center.
Ishmael, Stephen D. and McMonagle, Donald R. (1983) AFTI/F-16 Flight Test Results and Lessons. Technical Report NASA TM-84920, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick (1999) An H-Infinity Approach to Control Synthesis with Load Minimization for the F/A-18 Active Aeroelastic Wing. Conference Presentation NASA/CP-1999-209136/PT 1, Paper No. 3, Research Engineering, NASA Dryden Flight Research Center.
Hanson, Curtis E. and Ryan, Jack and Allen, Michael J. and Jacobson, Steven R. (2002) An Overview of Flight Test Results for a Formation Flight Autopilot. Technical Report NASA/TM-2002-210729, Research Engineeering, NASA Dryden Flight Research Center.
Kempel, Robert W. (1971) Analysis of a Coupled Roll-Spiral-Mode, Pilot-Induced Oscillation Experienced With the M2-F2 Lifting Body. Technical Report NASA Technical Note TN D-6496, Research Engineering, NASA Dryden Flight Research Center.
Smith, John W. (1981) Analysis of a Longitudinal Pilot-Induced Oscillation Experienced on the Approach and Landing Test of the Space Shuttle. Technical Report NASA TM-81366, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1978) Analytical Study of Ride Smoothing Benefits of Control System Configurations Optimized for Pilot Handling Qualities. Technical Report NASA TP-1148, Research Engineering, NASA Dryden Flight Research Center.
Antoniewicz, Robert F. and Duke, Eugene L. and Menon, P. K. A. (1991) Application and Flight Test of Linearizing Transformations Using Measurement Feedback to the Nonlinear Control Problem. Technical Report NASA TP-3154, Research Engineering, NASA Dryden Flight Research Center.
Sarrafian, Shahan K. and Powers, Bruce G. (1985) Application of Frequency Domain Handling Qualities Criteria to the Longitudinal Landing Task. Technical Report NASA TM-86728, Research Engineering, NASA Dryden Flight Research Center.
McRuer, Duane T. and Myers, Thomas T. and Hoh, Roger H. and Ashkenas, Irving L. and Johnston, Donald E. (1992) Assessment of Flying-Quality Criteria for Air-Breathing Aerospacecraft. Technical Report NASA CR-4442, Research Engineering, NASA Dryden Flight Research Center.
Allen, Michael J. (2005) Autonomous Soaring for Improved Endurance of a Small Uninhabited Air Vehicle. Meeting Presentation AIAA-2005-1025, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Stillwell, Wendell H. (1955) Behavior of the Bell X-1A Research Airplane During Exploratory Flights at Mach Numbers Near 2.0 and at Extreme Altitudes. Technical Report NACA RM H55G25, Research Engineering, NASA Dryden Flight Research Center.
Smith, John W. and Montgomery, Terry (1996) Biomechanically Induced and Controller Coupled Oscillations Experienced on the F-16XL Aircraft During Rolling Maneuvers. Technical Report NASA TM-4752, Research Engineering, NASA Dryden Flight Research Center.
Gupta, Kajal K. and Voelker, Leonard S. and Bach, Can and Doyle, Timothy and Hahn, Edward (2001) CFD-Based Aeroelastic Analysis of the X-43 Hypersonic Flight Vehicle. Meeting Paper AIAA-2001-0712, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. and Drake, Hubert M. and Fischel, Jack (1956) Comparison of Flight and Wind-Tunnel Measurements of High-Speed-Airplane Stability and Control Characteristics. Technical Report NACA TN 3859, Research Engineering, NASA Dryden Flight Research Center.
Privoznik, Cynthia M. and Berry, Donald T. (1986) Comparison of Pilot Effective Time Delay for Cockpit Controllers Used on Space Shuttle and Conventional Aircraft. Technical Report NASA TM-86030, Research Engineering, NASA Dryden Flight Research Center.
Burcham, Frank W. and Fullerton, C. Gordon (1991) Controlling Crippled Aircraft–With Throttles. Technical Report NASA TM-104238, Research Engineering, NASA Dryden Flight Research Center.
Day, Richard E. (1997) Coupling Dynamics in Aircraft: A Historical Perspective. NASA Special Publication SP-532, Research Engineering, NASA Dryden Flight Research Center. National Aeronautics and Space Administration.
Alag, Gurbux S. and Kempel, Robert W. and Pahle, Joseph W. (1986) Decoupling Control Synthesis For an Oblique-Wing Aircraft. Technical Report NASA TM-86801, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Antoniewicz, Robert F. and Krambeer, Keith D. (1988) Derivation and Definition of a Linear Aircraft Model. Technical Report NASA Reference Publication RP-1207, Research Engineering, NASA Ames Research Center Dryden Flight Research Facility.
McCarty, Craig A. and Feather, John B. and Dykman, John R. and Page, Mark A. and Hodgkinson, John (1992) Design and Analysis Issues of Integrated Control Systems for High-Speed Civil Transports. Technical Report NASA CR-186022, Research Engineering, NASA Dryden Flight Research Center.
Ishmael, Stephen D. and Regenie, Victoria A. and Mackall, Dale A. (1984) Design Implications From AFTI/F-16 Flight Test. Technical Report NASA TM-86026, Research Engineering, NASA Dryden Flight Research Center.
Smith, John W. and Edwards, John W. (1980) Design of a Nonlinear Adaptive Filter for Suppression of Shuttle Pilot-Induced Oscillation Tendencies. Technical Report NASA TM-81349, Research Engineering, NASA Dryden Flight Research Center.
Angle, Ellwyn E. and Holleman, Euclid C. (1950) Determination of Longitudinal Stability of the Bell X-1 Airplane from Transient Responses at Mach Numbers up to 1.12 at Lift Coefficients of 0.3 and 0.6. Technical Report NACA RM L50I06a, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel A. and Fullerton, C. Gordon and Webb, Lannie Dean (1996) Development and Flight Evaluation of an Emergency Digital Flight Control System Using Only Engine Thrust on an F-15 Airplane. Technical Report NASA TP-3627, Research Engineering, NASA Dryden Flight Research Center.
Mackall, Dale A. (1988) Development and Flight Test Experiences With a Flight-Crucial Digital Control System. Technical Report NASA TP-2857, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel A. and Burken, John J. and Pappas, Drew (1996) Development and Flight Test of an Augmented Thrust-Only Flight Control System on an MD-11 Transport Airplane. Technical Report NASA TM-4745, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Burken, John J. and Maine, Trindel A. and Fullerton, C. Gordon (1997) Development and Flight Test of an Emergency Flight Control System Using Only Engine Thrust on an MD-11 Transport Airplane. Technical Report NASA /TP-97-206217, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Burken, John J. (1980) Development and Flight Test Results of an Autothrottle Control System at Mach 3 Cruise. Technical Report NASA TP-1621, Research Engineering, NASA Dryden Flight Research Center.
Dibley, Ryan P. and Allen, Michael J. and Clarke, Robert and Gera, Joseph and Hodgkinson, John (2005) Development and Testing of Control Laws for the Active Aeroelastic Wing Program. Technical Report NASA/TM-2005-213666, Research Engineering, NASA Dryden Flight Research Center.
Dibley, Ryan P. and Allen, Michael J. and Clarke, Robert and Gera, Joseph and Hodgkinson, John (2005) Development and Testing of Control Laws for the Active Aeroelastic Wing Program. Conference Paper AIAA-2005-6314, Research Engineering, NASA Dryden Flight Research Center.
Duke, Eugene L. and Antoniewicz, Robert F. (1985) Development and Validation of a General Purpose Linearization Program for Rigid Aircraft Models. Technical Report NASA TM-86737, Research Engineering, NASA Dryden Flight Research Center.
Van Norman, Michael and Mackall, Dale A. (1986) Development Experience With a Simple Expert System Demonstrator for Pilot Emergency Procedures. Technical Report NASA TM-85919, Research Engineering, NASA Dryden Flight Research Center.
Alag, Gurbux S. and Duke, Eugene L. (1985) Development of a Flight Test Maneuver Autopilot for an F-15 Aircraft. Technical Report NASA TM-86799, Research Engineering, NASA Dryden Flight Research Center.
Alag, Gurbux Singh and Duke, Eugene L. (1985) Development of Control Laws for a Flight Test Maneuver Autopilot for an F-15 Aircraft. Technical Report NASA TM-86736, Research Engineering, NASA Dryden Flight Research Center.
Szalai, Kenneth J. and Jarvis, Calvin R. and Krier, Gary E. and Megna, Vincent A. and Brock, Larry D. and O'Donnell, Robert N. (1978) Digital Fly-By-Wire Flight Control Validation Experience. Technical Report NASA TM-72860, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. (1957) Dynamic Longitudinal Stability Characteristics of a Swept-Wing Fighter-Type Airplane at Mach Numbers Between 0.36 and 1.45. Technical Report NACA RM H56H03, Research Engineering, NASA Dryden Flight Research Center.
Gera, Joseph and Bosworth, John T. (1987) Dynamic Stability and Handling Qualities Tests on a Highly Augmented, Statically Unstable Airplane. Technical Report NASA TM-88297, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. and Iliff, Kenneth W. and Whitman, Robert K. (1978) Effect of Sampling Rate and Record Length on the Determination of Stability and Control Derivatives. Technical Report NASA TM-72858, Research Engineering, NASA Dryden Flight Research Center.
Fischel, Jack and Reisert, Donald (1955) Effect of Several Wing Modifications on the Low-Speed Stalling Characteristics of the Douglas D-558-II Research Airplane. Technical Report NACA RM H55E31a, Research Engineering, NASA Dryden Flight Research Center.
Fischel, Jack and Reisert, Donald (1956) Effect of Several Wing Modifications on the Subsonic and Transonic Longitudinal Handling Qualities of the Douglas D-558-II Research Airplane. Technical Report NACA RM H56C30, Research Engineering, NASA Dryden Flight Research Center.
Smith, Rogers E. and Sarrafian, Shahan K. (1986) Effect of Time Delay on Flying Qualities: An Update. Technical Report NASA TM-88264, Research Engineering, NASA Dryden Flight Research Center.
Mitchell, David G. and Aponso, Bimal L. and Klyde, David H. (1992) Effects of Cockpit Lateral Stick Characteristics on Handling Qualities and Pilot Dynamics. Technical Report NASA CR-4443, Research Engineering, NASA Dryden Flight Research Center.
Monaghan, Richard C. and Friend, Edward L. (1973) Effects of Flaps on Buffet Characteristics and Wing-Rock Onset of an F-8C Airplane at Subsonic and Transonic Speeds. Technical Report NASA TM X-2873, Research Engineering, NASA Dryden Flight Research Center.
Wagner, Charles A. (1994) Effects of Mass on Aircraft Sidearm Controller Characteristics. Technical Report NASA TM-104277, Research Engineering, NASA Dryden Flight Research Center.
Kern, Lura E. and Belle, Steve D. and Duke, Eugene L. (1990) Effects of Simplifying Assumptions on Optimal Trajectory Estimation for a High-Performance Aircraft. Technical Report NASA TM-101721, Research Engineering, NASA Dryden Flight Research Center.
Steers, Sandra Thornberry and Iliff, Kenneth W. (1975) Effects of Time-Shifted Data on Flight-Determined Stability and Control Derivatives. Technical Report NASA Technical Note TN D-7830, Research Engineering, NASA Dryden Flight Research Center.
Alag, Gurbux S. and Burken, John J. and Gilyard, Glenn B. (1986) Eigensystem Synthesis for Active Flutter Suppression on an Oblique-Wing Aircraft. Technical Report NASA TM-88275, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Carden, John R. (1950) Elevator-Stabilizer Effectiveness and Trim of the X-1 Airplane to a Mach Number of 1.06. Technical Report NACA RM L50G20, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Burken, John and Maine, Trindel A. and Bull, John (1997) Emergency Flight Control Using Only Engine Thrust and Lateral Center-of-Gravity Offset: A First Look. Technical Report NASA TM-4798, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Brenner, Marty and Haley, Sidney M. (1997) Estimation of Modal Parameters Using a Wavelet-Based Approach. Technical Report NASA/TM-97-206300, Research Engineering, NASA Dryden Flight Research Center.
Petersen, Kevin L. (1976) Evaluation of an Envelope-Limiting Device Using Simulation and Flight Test of a Remotely Piloted Research Vehicle. Technical Report NASA Technical Note TN D-8216, Research Engineering, NASA Dryden Flight Research Center.
Wilson, Ronald J. and Love, Betty J. and Larson, Richard R. (1971) Evaluation of Effects of High-Altitude Turbulence Encounters on the XB-70 Airplane. Technical Report NASA Technical Note TN D-6457, Research Engineering, NASA Dryden Flight Research Center.
Stoliker, Patrick C. and Bosworth, John T. (1996) Evaluation of High-Angle-of-Attack Handling Qualities for the X-31A Using Standard Evaluation Maneuvers. Technical Report NASA TM-104322, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Jackson, Dante W. (1997) Evaluation of High-Speed Civil Transport Handling Qualities Criteria With Supersonic Flight Data. Technical Report NASA TM-4791, Research Engineering, NASA Dryden Flight Research Center.
Sarrafian, Shahan K. (1984) Evaluation of HiMAT Aircraft Landing Approach Lateral Control Gearing Using Simulation and a Visual Display. Technical Report NASA TM-84916, Research Engineering, NASA Dryden Flight Research Center.
Mayer, Jann and Cox, Timothy H. (2003) Evaluation of Two Unique Side Stick Controllers in a Fixed-Base Flight Simulator. Technical Report NASA/TM-2003-212042, Research Engineering, NASA Dryden Flight Research Center.
Regenie, Victoria A. and Chacon, Claude V. and Lock, Wilton P. (1986) Experience with Synchronous and Asynchronous Digital Control Systems. Technical Report NASA TM-88271, Research Engineering, NASA Dryden Flight Research Center.
By Staff of the, Flight Research Center (1971) Experience With the X-15 Adaptive Flight Control System. Technical Report NASA Technical Note TN D-6208, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. (1973) Explicit Determination of Lateral-Directional Stability and Control Derivatives by Simultaneous Time Vector Analysis of Two Maneuvers. Technical Report NASA TM X-2722, Research Engineering, NASA Dryden Flight Research Center.
Andrews, William H. and Robinson, Glenn H. and Larson, Richard R. (1972) Exploratory Flight Investigation of Aircraft Response to The Wing Vortex Wake Generated by Jet Transport Aircraft. Technical Report NASA Technical Note TN D-6655, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Wang, Kon-Sheng Charles (1997) Extraction of Lateral-Directional Stability and Control Derivatives for the Basic F-18 Aircraft at High Angles of Attack. Technical Report NASA TM-4786, Research Engineering, NASA Dryden Flight Research Center.
Kukreja, Sunil L. (2007) F-15B Quiet Spike™ Aeroservoelastic Flight-Test Data Analysis. Technical Report NASA/TM-2007-214618, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. (1990) Flight Characteristics of a Modified Schweizer SGS 1-36 Sailplane at Low and Very High Angles of Attack. Technical Report NASA TP-3022, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. and Curry, Robert E. (1985) Flight Characteristics of the AD-1 Oblique-Wing Research Aircraft. Technical Report NASA Technical Paper TP-2223, Research Engineering, NASA Dryden Flight Research Center.
Kier, David A. (1970) Flight Comparison of Several Techniques for Determining the Minimum Flying Speed for a Large, Subsonic Jet Transport. Technical Report NASA Technical Note TN D-5806, Research Engineering, NASA Dryden Flight Research Center.
Friend, Edward L. and Sakamoto, Glenn M. (1978) Flight Comparison of the Transonic Agility of the F-111A Airplane and the F-111 Supercritical Wing Airplane. Technical Report NASA TP-1368, Research Engineering, NASA Dryden Flight Research Center.
Sitz, Joel R. and Vernon, Todd H. (1990) Flight Control System Design Factors for Applying Automated Testing Techniques. Technical Report NASA TM-4242, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and Earls, Michael R. (1988) Flight Control Systems Development and Flight Test Experience With the HiMAT Research Vehicles. Technical Report NASA Technical Paper TP-2822, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. and Walker, Joseph A. (1956) Flight Determination of the Lateral Handling Qualities of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H56C29, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. (1955) Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H55C07, Research Engineering, NASA Dryden Flight Research Center.
Gee, Shu W. and Gaidsick, Harold G. and Enevoldson, Einar K. (1971) Flight Evaluation of Angle of Attack as a Control Parameter in General-Aviation Aircraft. Technical Report NASA Technical Note TN D-6210, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Andrews, William H. and Darville, Robert W. (1957) Flight Evaluation of the Lateral Stability and Control Characteristics of the Convair YF-102 Airplane. Technical Report NACA RM H56G11, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and Dana, William H. and Sim, Alex G. (1975) Flight Evaluation of the M2-F3 Lifting Body Handling Qualities at Mach Numbers From 0.30 to 1.61. Technical Report NASA Technical Note TN D-8027, Research Engineering, NASA Dryden Flight Research Center.
Matheny, Neil W. and Gatlin, Donald H. (1978) Flight Evaluation of the Transonic Stability and Control Characteristics of an Airplane Incorporating a Supercritical Wing. Technical Report NASA TP-1167, Research Engineering, NASA Dryden Flight Research Center.
Weil, Joseph and Gates Jr., Ordway B. and Banner, Richard D. and Kuhl, Albert E. (1955) Flight Experience of Inertia Coupling in Rolling Maneuvers. Technical Report NACA RM H55E17b, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Andrews, William H. (1955) Flight Experience with a Delta-Wing Airplane Having Violent Lateral-Longitudinal Coupling in Aileron Rolls. Technical Report NACA RM H55H03, Research Engineering, NASA Dryden Flight Research Center.
Brown, S.R. and Szalai, K.J. (1977) Flight Experience with a Fail-Operational Digital Fly-By-Wire Control System. Conference Paper AIAA-1977-1507, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Smith, Mark S. and Morelli, Eugene A. (2003) Flight Investigation of Prescribed Simultaneous Independent Surface Excitations for Real-Time Parameter Identification. Technical Report NASA/TM-2003-212029, Research Engineering, NASA Dryden Flight Research Center.
Thompson, Jim Rogers and Roden, William S. and Eggelston, John M. (1950) Flight Investigation of the Aileron Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Between 0.6 and 0.89. Technical Report NACA RM L50D20, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. and Peele, James R. and Day, Richard E. (1956) Flight Investigation of the Effect of Vertical-Tail Size on the Rolling Behavior of a Swept-Wing Airplane Having Lateral-Longitudinal Coupling. Technical Report NACA RM H55L28a, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. and Powers, Bruce G. (1972) Flight Investigation of the Roll Requirements for Transport Airplanes in the Landing Approach. Technical Report NASA Technical Note TN D-7062, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. (1984) Flight Investigation of Various Control Inputs Intended for Parameter Estimation. Technical Report NASA TM-85901, Research Engineering, NASA Dryden Flight Research Center.
Friend, Edward L. and Sefic, Walter J. (1972) Flight Measurements of Buffet Characteristics of the F-104 Airplane for Selected Wing-Flap Deflections. Technical Report NASA Technical Note TN D-6943, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. and Finch, Thomas W. and Peele, James R. (1955) Flight Measurements of Directional Stability to a Mach Number of 1.48 for an Airplane Tested with Three Different Vertical Tail Configurations. Technical Report NACA RM H55G26, Research Engineering, NASA Dryden Flight Research Center.
Videan, Edward N. (1955) Flight Measurements of the Dynamic Lateral and Longitudinal Stability of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback. Technical Report NACA RM H55H10, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. (1955) Flight Measurements of the Lateral Response Characteristics of the Convair XF-92A Delta-Wing Airplane. Technical Report NACA RM H55E26, Research Engineering, NASA Dryden Flight Research Center.
Childs, Joan M. (1953) Flight Measurements of the Stability Characteristics of the Bell X-5 Research Airplane in Sideslips at 59 Degrees Sweepback. Technical Report NACA RM-L52K13b, Research Engineering, NASA Dryden Flight Research Center.
Wilmerding, J. V. and Stillwell, W. H. and Sjoberg, S. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Lateral Control Characteristics as Measured in Abrupt Aileron Rolls at Mach Numbers up to 0.86. Technical Report NACA RM L50E17, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, W. H. and Wilmerding, J. V. and Champine, R. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Low-Speed Stalling and Lift Characteristics. Technical Report NACA RM L50G10, Research Engineering, NASA Dryden Flight Research Center.
Sjoberg, S. A. (1950) Flight Measurements with the Douglas D-558-II (BuAero No. 37974) Research Airplane Static Lateral and Directional Stability Characteristics as Measured in Sideslips at Mach Numbers up to 0.87. Technical Report NACA RM L50C14, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. (2008) Flight Results of the NF-15B Intelligent Flight Control System (IFCS) Aircraft with Adaptation to a Longitudinally Destabilized Plant. Meeting Paper AIAA-2008-6985, Research and Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Cobleigh, Brent R. and Cox, Timothy H. and Conners, Timothy R. and Iliff, Kenneth W. and Powers, Bruce G. (1998) Flight Stability and Control and Performance Results from the Linear Aerospike SR-71 Experiment (LASRE). Technical Report NASA/TM-1998-206565, Research Engineering, NASA Dryden Flight Research Center.
Kempel, Robert W. and Horton, Timothy W. (1985) Flight Test Experience and Controlled Impact of a Large, Four-Engine, Remotely Piloted Airplane. Technical Report NASA TM-86738, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. and Smith, Rogers E. and Stewart, James F. and Bailey, Randall E. (1984) Flight Test Experience With Pilot-Induced-Oscillation Suppression Filters. Technical Report NASA TM-86028, Research Engineering, NASA Dryden Flight Research Center.
Williams-Hayes, Peggy S. (2005) Flight Test Implementation of a Second Generation Intelligent Flight Control System. Technical Report NASA/TM-2005-213669, Research Engineering, NASA Dryden Flight Research Center.
Williams-Hayes, Peggy S. (2005) Flight Test Implementation of a Second Generation Intelligent Flight Control System. Conference Presentation AIAA-2005-6995, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Burcham Jr., Frank W. and Maine, Trindel A. and Feather, John and Goldthorpe, Steven and Kahler, Jeffrey A. (1996) Flight Test of a Propulsion-Based Emergency Control System on the MD-11 Airplane With Emphasis on the Lateral Axis. Technical Report NASA TM-4746, Research Engineering, NASA Dryden Flight Research Center.
Deets, Dwain A. and Lock, Wilton P. and Megna, Vincent A. (1986) Flight Test of a Resident Backup Software System. Technical Report NASA TM-86807, Research Engineering, NASA Dryden Flight Research Center.
Clarke, Robert and Allen, Michael J. and Dibley, Ryan P. and Gera, Joseph and Hodgkinson, John (2005) Flight Test of the F/A-18 Active Aeroelastic Wing Airplane. Technical Report NASA/TM-2005-213664, Research Engineering, NASA Dryden Flight Research Center.
Clarke, Robert and Allen, Michael J. and Dibley, Ryan P. and Gera, Joseph and Hodgkinson, John (2005) Flight Test of the F/A-18 Active Aeroelastic Wing Airplane. Meeting Paper AIAA-2005-6316, Research Engineering, NASA Dryden Flight Research Center.
Bauer, Jeffrey E. and Clarke, Robert and Burken, John J. (1995) Flight Test of the X-29A at High Angle of Attack: Flight Dynamics and Controls. Technical Report NASA TP-3537, Research Engineering, NASA Dryden Flight Research Center.
Stachowiak, Susan J. and Bosworth, John T. (2004) Flight Test Results for the F-16XL With a Digital Flight Control System. Technical Report NASA/TP-2004-212046, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Williams-Hayes, Peggy S. (2007) Flight Test Results from the NF-15B Intelligent Flight Control System (IFCS) Project with Adaptation to a Simulated Stabilator Failure. Technical Report NASA/TM-2007-214629, Research and Engineering, NASA Dryden Flight Research Center.
Schkolnik, Gerard S. and Orme, John S. and Hreha, Mark A. (1995) Flight Test Validation of a Frequency-Based System Identification Method on an F-15 Aircraft. Technical Report NASA TM-4704, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., F. W. and Burken, John and Maine, Trindel A. (1994) Flight Testing a Propulsion-Controlled Aircraft Emergency Flight Control System on an F-15 Airplane. Technical Report NASA TM-4590, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel and Wolf, Thomas (1992) Flight Testing and Simulation of an F-15 Airplane Using Throttles for Flight Control. Technical Report NASA TM-104255, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. and Curry, Robert E. (1984) Flight-Determined Aerodynamic Derivatives of the AD-1 Oblique-Wing Research Airplane. Technical Report NASA Technical Paper TP-2222, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. (1972) Flight-Determined Derivatives and Dynamic Characteristics of the CV-990 Airplane. Technical Report NASA Technical Note TN D-6777, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. (1992) Flight-Determined Stability Analysis of Multiple-Input–Multiple-Output Control Systems. Technical Report NASA TM-4416, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex C. (1973) Flight-Determined Stability and Control Characteristics of the M2-F3 Lifting Body Vehicle. Technical Report NASA Technical Note TN D-7511, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. and Curry, Robert E. (1978) Flight-Determined Stability and Control Derivatives for the F-111 TACT Research Aircraft. Technical Report NASA Technical Paper TP-1350, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Wang, Kon-Sheng Charles (1997) Flight-Determined Subsonic Longitudinal Stability and Control Derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) With Thrust Vectoring. Technical Report NASA/TP-97-206539, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Burcham Jr., Frank W. (1997) Flight-Test Results of Propulsion-Only Emergency Control System on MD-11 Airplane. Journal of Guidance, Control, and Dynamics 20(5):980-987.
Davis, Mark C. and White, J. Terry (2006) Flight-Test-Determined Aerodynamic Force and Moment Characteristics of the X-43A at Mach 7.0. Meeting Presentation AIAA-2006-8028, Research Engineering, NASA Dryden Flight Research Center.
Stewart, James F. and Shuck, Thomas L. (1990) Flight-Testing of the Self-Repairing Flight Control System Using the F-15 Highly Integrated Digital Electronic Control Flight Research Facility. Technical Report NASA TM-101725, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Brenner, Marty (2000) Flutterometer: An On-Line Tool to Predict Robust Flutter Margins. Journal of Aircraft 37(6):1105-1112.
Carter, John F. and Stoliker, P. C. (2000) Flying Quality Analysis of a JAS 39 Gripen Ministick Controller in an F/A-18 Aircraft. Technical Report NASA/TM-2000-209024, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick (1999) Gain-Scheduled Approximations to H sub ∞ Controllers for the F/A-18 Active Aeroelastic Wing. Meeting Paper AIAA-1999-4205, Research Engineering, NASA Dryden Flight Research Center.
Allen, Michael J. and Lin, Victor (2007) Guidance and Control of an Autonomous Soaring UAV. Technical Report NASA/TM-2007-214611/REV1, Research and Engineering, NASA Dryden Flight Research Center.
Berry, Donald T. and Powers, Bruce G. (1970) Handling Qualities of the XB-70 Airplane in the Landing Approach. Technical Report NASA Technical Note TN D-5676, Research Engineering, NASA Dryden Flight Research Center.
Wichman, Keith D. and Pahle, Joseph W. and Bahm, Catherine and Davidson, John B. and Bacon, Barton J. and Murphy, Patrick C. and Ostroff, Aaron J. and Hoffler, Keith D. (1996) High-Alpha Handling Qualities Flight Research on the NASA F/A-18 High Alpha Research Vehicle. Technical Report NASA TM-4773, Research Engineering, NASA Dryden Flight Research Center.
Ray, J.K. and Carlin, C.M. and Lambregts, A.A. (1992) High-Speed Civil Transport Flight- and Propulsion-Control Technological Issues. Technical Report NASA CR-186015, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. and Montgomery, T. D. (1979) Important Factors in the Maximum Likelihood Analysis of Flight Test Maneuvers. Technical Report NASA TP-1459, Research Engineering, NASA Dryden Flight Research Center.
Berry, Donald T. (1985) In-Flight Evaluation of Pure Time Delays in Pitch and Roll. Technical Report NASA TM-86744, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. and Gilyard, Glenn B. (1971) In-Flight Evaluation of the Lateral Handling of a Four-Engine Jet Transport During Approach and Landing. Technical Report NASA Technical Note TN D-6339, Research Engineering, NASA Dryden Flight Research Center.
Regan, Christopher D. (2008) In-Flight Stability Analysis of the X-48B Aircraft. Meeting Paper AIAA-2008-6571, Research and Engineering, NASA Dryden Flight Research Center.
Curry, Robert E. and Sim, Alex G. (1984) In-Flight Total Forces, Moments, and Static Aeroelastic Characteristics of an Oblique-Wing Research Airplane. Technical Report NASA TP-2224, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. and Koehler, Ruthard and Wilson, Edward M. and Levy, David R. (1989) Initial Flight Test of a Ground Deployed System for Flying Qualities Assessment. Technical Report NASA TM-101700, Research Engineering, NASA Dryden Flight Research Center.
Carter, John and Stephenson, Mark (1999) Initial Flight Test of the Production Support Flight Control Computers at NASA Dryden Flight Research Center. Technical Report NASA/TM-1999-206581, Research Engineering, NASA Dryden Flight Research Center.
Carter, John and Stephenson, Mark (1999) Initial Flight Test of the Production Support Flight Control Computers at NASA Dryden Flight Research Center. Meeting Paper AIAA-1999-4203, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Gilyard, Glenn B. and Gelhausen, Paul A. (1990) Integrated Flight-Propulsion Control Concepts for Supersonic Transport Airplanes. Technical Report NASA TM-101728, Research Engineering, NASA Dryden Flight Research Center.
Hageman, Jacob J. and Smith, Mark S. and Stachowiak, Susan (2003) Integration of Online Parameter Identification and Neural Network for In-Flight Adaptive Control. Technical Report NASA/TM-2003-212028, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Muhleman, Duane O. (1955) Lateral Stability and Control Characteristics of the Convair XF-92A Delta-Wing Airplane as Measured in Flight. Technical Report NACA RM H55A17, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. (1948) Limited Measurements of Static Longitudinal Stability in Flight of Douglas D-558-I Airplane. Technical Report NACA RM L8E14, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. (1992) Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison With Flight Data. Technical Report NASA TM-4356, Research Engineering, NASA Dryden Flight Research Center.
Stoliker, Patrick C. and Bosworth, John T. and Georgie, Jennifer (1997) Linearized Poststall Aerodynamic and Control Law Models of the X-31A Aircraft and Comparison with Flight Data. Technical Report NASA/TM-97-206318, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. and Yancey, Roxanah B. (1972) Longitudinal Aerodynamic Characteristics of Light, Twin-Engine, Propeller-Driven Airplanes. Technical Report NASA Technical Note TN D-6800, Research Engineering, NASA Dryden Flight Research Center.
Andrews, William H. and Sisk, Thomas R. and Darville, Robert W. (1956) Longitudinal Stability Characteristics of the Convair YF-102 Airplane Determined from Flight Tests. Technical Report NACA RM H56I17, Research Engineering, NASA Dryden Flight Research Center.
Sadoff, Melvin and Sisk, Thomas R. (1950) Longitudinal-Stability Characteristics of the Northrop X-4 Airplane (USAF No. 46-677). Technical Report NACA RM A50D27, Research Engineering, NASA Dryden Flight Research Center.
Kock, Berwin M. and Fulton Jr, Fitzhugh L. and Drinkwater III, Fred J. (1972) Low-Lift-To-Drag-Ratio Approach and Landing Studies Using a CV-990 Airplane. Technical Report NASA Technical Note TN D-6732, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Fullerton, C. Gordon and Maine, Trindel A. (2004) Manual Manipulation of Engine Throttles for Emergency Flight Control. Technical Report NASA/TM-2004-212045, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1949) Measured Characteristics of the Douglas D-558-I Airplane (BuAero No. 37971) in Two Landings. Technical Report NACA RM L9D20a, Research Engineering, NASA Dryden Flight Research Center.
Alag, Gurbux S. and Kempel, Robert W. and Pahle, Joseph W. and Bresina, John J. and Bartoli, Febo (1986) Model-Following Control for an Oblique-Wing Aircraft. Technical Report NASA TM-88269, Research Engineering, NASA Dryden Flight Research Center.
Sim, Alex G. (1991) Modeling, Simulation, and Flight Characteristics of an Aircraft Designed to Fly at 100,000 Feet. Technical Report NASA TM-104326, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. (1985) More Than You May Want To Know About Maximum Likelihood Estimation. Technical Report NASA TM-85905, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. and Thompson Ph.D., Peter M. and Klyde, David H. and Bachelder Ph.D., Edward N. and Rosenthal, Theodore J. (2005) On-Line Loss of Control Detection Using Wavelets. Technical Report NASA/CR-2005-212873, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. and Lind, Rick (1998) On-Line Robust Modal Stability Prediction Using Wavelet Processing. Technical Report NASA/TM-1998-206550, Research Engineering, NASA Dryden Flight Research Center.
Pahle, Joseph W. (1990) Output Model-Following Control Synthesis for an Oblique-Wing Aircraft. Technical Report NASA TM-100454, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1977) Phugoid Charcteristics of a YF-12 Airplane with Variable-Geometry Inlets Obtained in Flight Tests at a Mach Number of 2.9. Technical Report NASA TP-1107, Research Engineering, NASA Dryden Flight Research Center.
Shafer, Mary F. and Steinmetz, Paul (2001) Pilot-Induced Oscillation Research: Status at the End of the Century. Conference Proceedings Report NASA/CP-2001-210389/VOL1, Pilot-Induced Oscillation Research: The Status at the End of the Century, NASA Dryden Flight Research Center.
Shafer, Mary F. and Steinmetz, Paul (2001) Pilot-Induced Oscillation Research: Status at the End of the Century. Conference Proceedings Report NASA/CP-2001-210389/VOL2, Pilot-Induced Oscillation Research: Status at the End of the Century, NASA Dryden Flight Research Center.
Shafer, Mary F. and Steinmetz, Paul (2001) Pilot-Induced Oscillation Research: Status at the End of the Century. Conference Proceedings Report NASA/CP-2001-210389/VOL3, Pilot-Induced Oscillation Research: Status at the End of the Century, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. (1976) Practical Aspects of Using a Maximum Likelihood Estimation Method to Extract Stability and Control Derivatives From Flight Data. Technical Report NASA Technical Note TN D-8209, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Matheny, Neil W. (1979) Precision Controllability of the F-15 Airplane. Technical Report NASA TM-72861, Research Engineering, NASA Dryden Flight Research Center.
Sisk, Thomas R. and Matheny, Neil W. (1980) Precision Controllability of the YF-17 Airplane. Technical Report NASA TP-1677, Research Engineering, NASA Dryden Flight Research Center.
Friend, Edward L. and Matheny, Neil W. (1977) Preliminary Flight Measurements of the Buffet Characteristics of Prototype Lightweight Fighter Aircraft. Technical Report NASA TM X-3549, Research Engineering, NASA Dryden Flight Research Center.
Burcham, Frank W. and Maine, Trindel A. and Fullerton, C. Gordon and Wells, Edward A. (1993) Preliminary Flight Results of a Fly-by-Throttle Emergency Flight Control System on an F-15 Airplane. Technical Report NASA TM-4503, Research Engineering, NASA Dryden Flight Research Center.
Sjoberg, Sigurd A. (1949) Preliminary Measurements of the Dynamic Lateral Stability Characteristics of the Douglas D-558-II (BuAero No. 37974) Airplane. Technical Report NACA RM L9G18, Research Engineering, NASA Dryden Flight Research Center.
Finch, Thomas W. and Briggs, Donald W. (1953) Preliminary Results of Stability and Control Investigation of the Bell X-5 Research Airplane. Technical Report NACA RM-L52K18b, Research Engineering, NASA Dryden Flight Research Center.
Hodge, Kenneth E. (Compiled by) (1996) Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration, Volume I. Technical Report NASA Conference Publication CP-3256, Volume I, Research Engineering, NASA Dryden Flight Research Center.
Hodge, Kenneth E. (Compiled by) (1996) Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration, Volume II. Technical Report NASA Conference Publication CP-3256, Volume II, Research Engineering, NASA Dryden Flight Research Center.
Smith, Mark S. and Moes, Timothy R. and Morelli, Eugene A. (2003) Real-Time Stability and Control Derivative Extraction From F-15 Flight Data. Technical Report NASA/TM-2003-212027, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Stachowiak, Susan J. (2005) Real-Time Stability Margin Measurements for X-38 Robustness Analysis. Technical Report NASA/TP-2005-212856, Research Engineering, NASA Dryden Flight Research Center.
Cotting, M. Christopher and Burken, John J. (2001) Reconfigurable Control Design for the Full X-33 Flight Envelope. Technical Report NASA/TM-2001-210396, Research Engineering, NASA Dryden Flight Research Center.
Cotting, M. Christopher and Burken, John J. (2001) Reconfigurable Control Design for the Full X-33 Flight Envelope. Meeting Paper AIAA-2001-4379, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Williams-Hayes, Peggy and Kaneshige, John T. and Stachowiak, Susan J. (2006) Reconfigurable Control with Neural Network Augmentation for a Modified F-15 Aircraft. Technical Report NASA/TM-2006-213678, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Lu, Ping and Wu, Zhenglu (1999) Reconfigurable Flight Control Designs With Application to the X-33 Vehicle. Technical Report NASA TM-1999-206582, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Lu, Ping and Wu, Zhenglu (1999) Reconfigurable Flight Control Designs with Application to the X-33 Vehicle. Meeting Paper AIAA-1999-4134, Research Engineering, NASA Dryden Flight Research Center.
Pahle, Joseph W. and Powers, Bruce and Regenie, Victoria and Chacon, Vince and Degroote, Steve and Murnyak, Steven (1991) Research Flight-Control System Development for the F-18 High Alpha Research Vehicle. Technical Report NASA TM-104232, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Noffz, Gregory K. and Iliff, Kenneth W. (2000) Results From F-18B Stability and Control Parameter Estimation Flight Tests at High Dynamic Pressures. Technical Report NASA/TP-2000-209033, Research Engineering, NASA Dryden Flight Research Center.
Gilyard, Glenn B. and Smith, John W. (1978) Results From Flight and Simulator Studies of a Mach 3 Cruise Longitudinal Autopilot. Technical Report NASA TP-1180, Research Engineering, NASA Dryden Flight Research Center.
Matthews Jr., James T. (1950) Results Obtained During Flights 1 to 6 of the Northrop X-4 Airplane (A.F. No. 46-677). Technical Report NACA RM L9K22, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. (1949) Results Obtained from Second Flight of X-4 Airplane (A.F. No. 46-676). Technical Report NACA RM L9F21, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. (1949) Results Obtained from Third Flight of Northrop X-4 Airplane (A.F. 46-676). Technical Report NACA RM L9G20a, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Brenner, Martin J. (1998) Robust Flutter Margin Analysis That Incorporates Flight Data. Technical Report NASA/TP-1998-206543, Research Engineering, NASA Dryden Flight Research Center.
Williams-Hayes, Peggy S. (2004) Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System. Technical Report NASA/TM-2004-212857, Research Engineering, NASA Dryden Flight Research Center.
Williams, Peggy S. (2004) Selected Flight Test Results for Online Learning Neural Network-Based Flight Control System. Meeting Paper AIAA-2004-6283, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. and Sarrafian, Shahan K. (1986) Simulation Studies of Alternate Longitudinal Control Systems for the Space Shuttle Orbiter in the Landing Regime. Technical Report NASA TM-86815, Research Engineering, NASA Dryden Flight Research Center.
Sarrafian, Shahan K. (1984) Simulator Evaluation of a Remotely Piloted Vehicle Lateral Landing Task Using a Visual Display. Technical Report NASA TM-85903, Research Engineering, NASA Dryden Flight Research Center.
Burcham Jr., Frank W. and Maine, Trindel A. and Kaneshige, John and Bull, John (1999) Simulator Evaluation of Simplified Propulsion-Only Emergency Flight Control Systems on Transport Aircraft. Technical Report NASA/TM-1999-206578, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, Wendell H. and Drake, Hubert M. (1958) Simulator Studies of Jet Reaction Controls For Use at High Altitude. Technical Report NACA RM H58G18A, Research Engineering, NASA Dryden Flight Research Center.
Fisher, David F. (2007) Six Decades of Flight Research: An Annotated Bibliography of Technical Publications of NASA Dryden Flight Research Center, 1946-2006. Technical Report NASA/TP-2007-213684, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. and Drake, Hubert M. and Fischel, Jack (1956) Some Correlations of Flight-Measured and Wind-Tunnel Measured Stability and Control Characteristics of High-Speed Airplanes. Technical Report NACA H56AG62, Research Engineering, NASA Dryden Flight Research Center.
Williams, Walter C. and Phillips, William H. (1956) Some Recent Research on the Handling Qualities of Airplanes. Technical Report NACA RM H55L29a, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1984) Space Shuttle Pilot-Induced-Oscillation Research Testing. Technical Report NASA TM-86034, Research Engineering, NASA Dryden Flight Research Center.
Day, Richard E. and Fischel, Jack (1955) Stability and Control Characteristics Obtained During Demonstration of the Douglas X-3 Research Airplane. Technical Report NACA RM H55E16, Research Engineering, NASA Dryden Flight Research Center.
Drake, Hubert M. (1949) Stability and Control Data Obtained from First Flight of X-4 Airplane. Technical Report NACA RM L9A31, Research Engineering, NASA Dryden Flight Research Center.
Valentine, George M. (1949) Stability and Control Data Obtained from Fourth and Fifth Flights of the Northrop X-4 Airplane (A.F. No. 46-676). Technical Report NACA RM L9G25a, Research Engineering, NASA Dryden Flight Research Center.
Tanner, Russel R. and Montgomery, Terry D. (1979) Stability and Control Derivative Estimates Obtained from Flight Data for the Beech 99 Aircraft. Technical Report NASA TM-72863, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Iliff, Kenneth (2002) Stability and Control Estimation Flight Test Results for the SR-71 Aircraft With Externally Mounted Experiments. Technical Report NASA/TP-2002-210718, Research Engineering, NASA Dryden Flight Research Center.
Moua, Cheng M. and Cox, Timothy H. and McWherter, Shaun C. (2008) Stability and Controls Analysis and Flight Test Results of a 24-Foot Telescoping Nose Boom on an F-15B Airplane. Meeting Presentation AIAA-2008-0126, Research and Engineering, NASA Dryden Flight Research Center.
Barlow, William H. and Lilly, Howard C. (1949) Stability Results Obtained with Douglas D-558-I Airplane (BuAero No. 37971) in Flight up to a Mach Number of 0.89. Technical Report NACA RM L8K03, Research Engineering, NASA Dryden Flight Research Center.
Sadoff, Melvin and Sisk, Thomas R. (1950) Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677). Technical Report NACA RM A50A04, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1972) Statistical Survey of XB-70 Airplane Responses and Control Usage With an Illustration of the Application to Handling Qualities Criteria. Technical Report NASA Technical Note TN D-6872, Research Engineering, NASA Dryden Flight Research Center.
Reukauf, Paul J. and Burcham Jr., Frank W. and Holzman, Jon K. (1975) Status of a Digital Integrated Propulsion/Flight Control System for the YF-12 Airplane. Conference Paper AIAA-1975-1180, Research Engineering, NASA Dryden Flight Research Center.
Allen, Michael J. and Ryan, Jack and Parle, James F. and Hanson, Curtis E. (2002) String Stability of a Linear Formation Flight Control System. Technical Report NASA/TM-2002-210733, Research Engineering, NASA Dryden Flight Research Center.
Powers, Bruce G. (1996) Structural Dynamic Model Obtained From Flight for Use With Piloted Simulation and Handling Qualities Analysis. Technical Report NASA TM-4747, Research Engineering, NASA Dryden Flight Research Center.
Stillwell, Wendell H. (1956) Studies of Reaction Controls. Technical Report NACA-CONF-26-Oct-56-p175-181, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Maine, Richard E. and Shafer, Mary F. (1976) Subsonic Stability and Control Derivatives for an Unpowered, Remotely Piloted 3/8-Scale F-15 Airplane Model Obtained From Flight Test. Technical Report NASA Technical Note TN D-8136, Research Engineering, NASA Dryden Flight Research Center.
Holleman, Euclid C. (1976) Summary of Flight Tests to Determine the Spin and Controllability Characteristics of a Remotely Piloted, Large-Scale (3/8) Fighter Airplane Model. Technical Report NASA Technical Note TN D-8052, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. and Yancey, Roxanah B. (1973) Summary of Stability and Control Characteristics of the XB-70 Airplane. Technical Report NASA TM X-2933, Research Engineering, NASA Dryden Flight Research Center.
Walsh, Kevin R. (1993) Summary of the Effects of Engine Throttle Response on Airplane Formation-Flying Qualities. Technical Report NASA TM-4465, Research Engineering, NASA Dryden Flight Research Center.
Sadoff, Melvin and Sisk, Thomas R. (1950) Summary Report of Results Obtained During Demonstration Tests of the Northrop X-4 Airplanes. Technical Report NACA RM A50I01, Research Engineering, NASA Dryden Flight Research Center.
Cox, Timothy H. and Jackson, Dante (1997) Supersonic Flying Qualities Experience Using the SR-71. Technical Report NASA TM-4800, Research Engineering, NASA Dryden Flight Research Center.
Baumann, Ethan (2007) Tailored Excitation for Frequency Response Measurement Applied to the X-43A Flight Vehicle. Technical Report NASA/TM-2007-214609, Research and Engineering, NASA Dryden Flight Research Center.
Baumann, Ethan (2006) Tailored Excitation for Frequency Response Measurement Applied to the X-43A Flight Vehicle. Meeting Presentation AIAA-2006-638, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Burken, John J. (1997) Tailored Excitation for Multivariable Stability-Margin Measurement Applied to the X-31A Nonlinear Simulation. Technical Report NASA TM-113085, Research Engineering, NASA Dryden Flight Research Center.
Love, James E. and Stillwell, Wendell H. (1959) The Hydrogen-Peroxide Rocket Reaction-Control System for the X-1B Research Airplane. Technical Report NASA Technical Note TN D-185, Research Engineering, NASA Dryden Flight Research Center.
Corda, Stephen and Moes, Timothy R. and Mizukami, Masashi and Hass, Neal E. and Jones, Daniel and Monaghan, Richard C. and Ray, Ronald J. and Jarvis, Michele L. and Palumbo, Nathan (2000) The SR-71 Test Bed Aircraft: A Facility for High-Speed Flight Research. Technical Report NASA/TP-2000-209023, Research Engineering, NASA Dryden Flight Research Center.
Bosworth, John T. and Stoliker, P. C. (1996) The X-31A Quasi-Tailless Flight Test Results. Technical Report NASA TP-3624, Research Engineering, NASA Dryden Flight Research Center.
Bahm, Catherine and Baumann, Ethan and Martin, John and Bose, David and Beck, Roger E. and Strovers, Brian (2005) The X-43A Hyper-X Mach 7 Flight 2 Guidance, Navigation, and Control Overview and Flight Test Results. Conference Presentation AIAA-2005-3275, Research Engineering, NASA Dryden Flight Research Center.
Peron, Lee R. and Carpenter, Thomas (1992) Thrust Vectoring for Lateral-Directional Stability. Technical Report NASA CR-186016, Research Engineering, NASA Dryden Flight Research Center.
Wolowicz, Chester H. (1956) Time-Vector Determined Lateral Derivatives of a Swept-Wing Fighter-Type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48. Technical Report NACA RM H56C20, Research Engineering, NASA Dryden Flight Research Center.
Burken, John J. and Lu, Ping and Wu, Zhenglu and Bahm, Cathy (2001) Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation. Journal of Guidance, Control, and Dynamics 24(3):482-493.
Szalai, Kenneth J. (1971) Validation of a General Purpose Airborne Simulator For Simulation of Large Transport Aircraft Handling Qualities. Technical Report NASA Technical Note TN D-6431, Research Engineering, NASA Dryden Flight Research Center.
Berry, Donald T. and Sarrafian, Shahan K. (1986) Validation of a New Flying Quality Criterion for the Landing Task. Technical Report NASA TM-88261, Research Engineering, NASA Dryden Flight Research Center.
Smith, John W. and Lock, Wilton P. and Payne, Gordon A. (1992) Variable-Camber Systems Integration and Operational Performance of the AFTI/F-111 Mission Adaptive Wing. Technical Report NASA TM-4370, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Martin J. (1997) Wavelet Analyses of F/A-18 Aeroelastic and Aeroservoelastic Flight Test Data. Technical Report NASA TM-4793, Research Engineering, NASA Dryden Flight Research Center.
Brenner, Marty and Lind, Rick (1998) Wavelet Filtering To Reduce Conservatism In Aeroservoelastic Robust Stability Margins. Technical Report NASA/TM-1998-206545, Research Engineering, NASA Dryden Flight Research Center.
Lind, Rick and Brenner, Marty (1997) Worst-Case Flutter Margins from F/A-18 Aircraft Aeroelastic Data. Conference Paper AIAA-97-1266, Research Engineering, NASA Dryden Flight Research Center.
Clarke, Robert and Burken, John J. and Bosworth, John T. and Bauer, Jeffrey E. (1994) X-29 Flight Control System: Lessons Learned. Technical Report NASA TM-4598, Research Engineering, NASA Dryden Flight Research Center.
Iliff, Kenneth W. and Wang, Kon-Sheng Charles (1996) X-29A Lateral–Directional Stability and Control Derivatives Extracted From High-Angle-of-Attack Flight Data. Technical Report NASA TP-3664, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Wed Aug 27 18:15:30 PDT 2008.
