Subject: (06) Avionics And Aircraft Instrumentation
Number of records: 67.
Enevoldson, Einar K. and Horton, Victor W. (1981) "Light Bar" Attitude Indicator. Conference Paper, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Whitmore, Stephen A. (1990) A Preliminary Look at Techniques Used to Obtain Airdata From Flight at High Angles of Attack. Technical Report NASA TM-101729, Research Engineering, NASA Dryden Flight Research Center.
Jenkins, Jerald M. (1983) A Study of the Effect of Apparent Strain on Thermal Stress Measurement for Two Types of Elevated Temperature Strain Gages. Technical Report NASA TM-84904, Research and Engineering, NASA Dryden Flight Research Center.
Sakamoto, Glenn M. (1976) Aerodynamic Characteristics of a Vane Flow Angularity Sensor System Capable of Measuring Flightpath Accelerations for the Mach Number Range From 0.40 to 2.54. Technical Report NASA Technical Note TN D-8242, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Larson, Terry J. and Ehernberger, L.J. (1984) Air Data Position-Error Calibration Using State Reconstruction Techniques. Technical Report NASA TM-86029, Research Engineering, NASA Dryden Flight Research Center.
Soreide, David C. and Bogue, Rodney K. and Ehernberger, L.J. and Hannon, Stephen M. and Bowdle, David A. (2000) Airborne Coherent Lidar for Advanced In-Flight Measurements (ACLAIM) Flight Testing of the Lidar Sensor. Meeting Paper AMS Paper 8.18, Research Engineering, NASA Dryden Flight Research Center.
Wilner, Douglass O. and Bever, Glenn A. (1984) An Automated Stall-Speed Warning System. Technical Report NASA TM-84917, Research Engineering, NASA Dryden Flight Research Center.
Veatch, Donald W. and Bogue, Rodney K. (1986) Analog Signal Conditioning for Flight-Test Instrumentation. Technical Report NASA Reference Publication RP-1159, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Moes, Timothy R. and Czerniejewski, Mark W. and Nichols, Douglas A. (1993) Application of a Flush Airdata Sensing System to a Wing Leading Edge (LE-FADS). Technical Report NASA TM-104267, Research Engineering, NASA Dryden Flight Research Center.
Soreide, David and Bogue, Rodney K. and Ehernberger, L.J. and Bagley, Hal (1996) Coherent Lidar Turbulence Measurement for Gust Load Alleviation. Technical Report NASA TM-104318, Research Engineering, NASA Dryden Flight Research Center.
Bogue, Rodney and McGann, Rick and Wagener, Thomas and Abbiss, John and Smart, Anthony (1997) Comparative Optical Measurements of Airspeed and Aerosols on a DC-8 Aircraft. Technical Report NASA TM-113083, Research Engineering, NASA Dryden Flight Research Center.
Hamory, Philip J. and Diamond, John K. and Bertelrud, Arild (1999) Design and Calibration of an Airborne Multichannel Swept-Tuned Spectrum Analyzer. Technical Report NASA/TM-1999-206584, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Cobleigh, Brent R. and Haering, Edward A. (1998) Design and Calibration of the X-33 Flush Airdata Sensing (FADS) System. Technical Report NASA/TM-1998-206540, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Fife, Mike and Brashear, Logan (1997) Development of a Closed-Loop Strap Down Attitude System for an Ultrahigh Altitude Flight Experiment. Technical Report NASA TM-4775, Research Engineering, NASA Dryden Flight Research Center.
Davis, Mark C. and Pahle, Joseph W. and White, John Terry and Marshall, Laurie A. and Mashburn, Michael J. and Franks, Rick (2000) Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8. Technical Report NASA/TM-2000-209017, Research Engineering, NASA Dryden Flight Research Center.
Davis, Mark C. and Pahle, Joseph W. and White, John Terry and Marshall, Laurie A. and Mashburn, Michael J. and Franks, Rick (2000) Development of a Flush Airdata Sensing System on a Sharp-Nosed Vehicle for Flight at Mach 3 to 8. Meeting Paper AIAA-2000-0504, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. (1991) Development of a Pneumatic High-Angle-of-Attack Flush Airdata Sensing (HI-FADS) System. Technical Report NASA TM-104241, Research Engineering, NASA Dryden Flight Research Center.
Chiles, Harry R. and Johnson, J. Blair (1985) Development of a Temperature-Compensated Hot-Film Anemometer System for Boundary-Layer Transition Detection on High-Performance Aircraft. Technical Report NASA TM-86732, Research Engineering, NASA Dryden Flight Research Center.
Bever, Glenn A. (1991) Digital Signal Conditioning for Flight Test Instrumentation. Technical Report NASA TM-101739, Research Engineering, NASA Dryden Flight Research Center.
Harney, Paul F. (1981) Diversity Techniques for Omnidirectional Telemetry Coverage of The HiMAT Research Vehicle. Technical Report NASA TP-1830, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Lindsey, William T. and Curry, Robert E. and Gilyard, Glenn B. (1990) Experimental Characterization of the Effects of Pneumatic Tubing on Unsteady Pressure Measurements. Technical Report NASA TM-4171, Research Engineering, NASA Dryden Flight Research Center.
Nugent, Jack and Couch, Lana M. and Webb, Lannie D. (1975) Exploratory Wind Tunnel Tests of a Shock-Swallowing Air Data Sensor at a Mach Number of Approximately 1.83. Technical Report NASA TM X-56030, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Moes, Timothy R. (1992) Failure Detection and Fault Management Techniques for a Pneumatic High-Angle-of-Attack Flush Airdata Sensing (HI-FADS) System. Technical Report NASA TM-4335, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Whitmore, Stephen A. and Jordan Jr., Frank L. (1993) Flight and Wind-Tunnel Calibrations of a Flush Airdata Sensor at High Angles of Attack and Sideslip and at Supersonic Mach Numbers. Technical Report NASA TM-104265, Research Engineering, NASA Dryden Flight Research Center.
Webb, Lannie D. and Washington, Harold P. (1972) Flight Calibration of Compensated and Uncompensated Pitot-Static Airspeed Probes and Application of the Probes to Supersonic Cruise Vehicles. Technical Report NASA Technical Note TN D-6827, Research Engineering, NASA Dryden Flight Research Center.
Thompson, Jim Rogers and Bray, Richard S. and Cooper, George E. (1955) Flight Calibration of Four Airspeed Systems on a Swept-Wing Airplane at Mach Numbers up to 1.04 by the NACA Radar-Phototheodolite Method. Technical Report NACA TN 3526, Research Engineering, NASA Dryden Flight Research Center.
Armistead, Katharine H. and Webb, Lannie D. (1973) Flight Calibration Tests of a Nose-Boom-Mounted Fixed Hemispherical Flow-Direction Sensor. Technical Report NASA Technical Note TN D-7461, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Sarma, Garimella R. and Mangalam, Siva M. (1997) Flight Demonstration of a Shock Location Sensor Using Constant Voltage Hot-Film Anemometry. Technical Report NASA TM-4806, Research Engineering, NASA Dryden Flight Research Center.
Schweikhard, Keith A. and Richards, W. Lance and Theisen, John and Mouyos, William and Garbos, Raymond (2001) Flight Demonstration of X-33 Vehicle Health Management System Components on the F/A-18 Systems Research Aircraft. Technical Report NASA/TM-2001-209037, Research Engineering, NASA Dryden Flight Research Center.
Hamory, Philip J. and Murray, James E. (1993) Flight Experience With Lightweight, Low-Power Miniaturized Instrumentation Systems. Technical Report NASA TM-4463, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. and Whitmore, Stephen A. and Haering Jr., Edward A. and Borrer, Jerry and Roback, V. Eric (1999) Flush Airdata Sensing (FADS) System Calibration Procedures and Results for Blunt Forebodies. Technical Report NASA/TP-1999-209012, Research Engineering, NASA Dryden Flight Research Center.
Cobleigh, Brent R. and Whitmore, Stephen A. and Haering Jr., Edward A. and Borrer, Jerry and Roback, V. Eric (1999) Flush Airdata Sensing (FADS) System Calibration Procedures and Results for Blunt Forebodies. Meeting Paper AIAA-1999-4816, Research Engineering, NASA Dryden Flight Research Center.
Wolf, Thomas D. and McCracken, Robert C. (1973) Ground and Flight Experience with a Strapdown Inertial Measuring Unit and a General Purpose Airborne Digital Computer. Technical Report NASA TM X-2848, Research Engineering, NASA Dryden Flight Research Center.
Mangalam, Arun S. and Davis, Mark C. (2009) Ground/Flight Correlation of Aerodynamic Loads with Structural Response. Technical Report NASA/TM-2009-214644, Research and Engineering, NASA Dryden Flight Research Center.
Mangalam, Arun S. and Davis, Mark C. (2009) Ground/Flight Correlation of Aerodynamic Loads with Structural Response. Meeting Paper AIAA-2009-0881, Research and Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Heeg, Jennifer and Larson, Terry J. and Ehernberger, L.J. and Hagen, Floyd W. and DeLeo, Richard V. (1987) High-Anqle-of-Attack Pneumatic Lag and Upwash Corrections for a Hemispherical Flow Direction Sensor. Technical Report NASA TM-86790, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Davis, Roy J. and Fife, John Michael (1995) In-Flight Demonstration of a Real-Time Flush Airdata Sensing (RT–FADS) System. Technical Report NASA TM-104314, Research Engineering, NASA Dryden Flight Research Center.
Richwine, David M. and Fisher, David F. (1992) In-Flight Leading Edge Extension Vortex Flow-Field Survey Measurements on a F-18 Aircraft at High Angle of Attack. Technical Report NASA TM-4398, Research Engineering, NASA Dryden Flight Research Center.
Taback, I. and Truszynski, G. M. (1956) Instrumentation for the X-15. Technical Report NACA-CONF-26-Oct-56-p183-191, Research Engineering, NASA Dryden Flight Research Center.
Brunn, Cyril D. and Stillwell, Wendell H. (1956) Mach Number Measurements and Calibrations During Flight at High Speeds and at High Altitudes Including Data for the D-558-II Research Airplane. Technical Report NACA RM H55J18, Research Engineering, NASA Dryden Flight Research Center.
Enevoldson, Einar K. (1984) NASA Ames-Dryden T-37 Demonstration Comments.
Bogue, Rodney K. and Jentink, Henk W. (2004) Optical Air Flow Measurements in Flight. Technical Report NASA/TP-2004-210735, Research Engineering, NASA Dryden Flight Research Center.
Bertelrud, Arild and de la Tova, Geva and Hamory, Philip J. and Young, Ronald and Noffz, Gregory K. and Dodson, Michael and Graves, Sharon S. and Diamond, John K. and Bartlett, James E. and Noack, Robert and Knoblock, David (2000) Pegasus® Wing-Glove Experiment to Document Hypersonic Crossflow Transition-Measurement System and Selected Flight Results. Meeting Paper AIAA-2000-0505, Research Engineering, NASA Dryden Flight Research Center.
Bertelrud, Arild and de la Tova, Geva and Hamory, Philip J. and Young, Ronald and Noffz, Gregory K. and Dodson, Michael and Graves, Sharon S. and Diamond, John K. and Bartlett, James E. and Noack, Robert and Knoblock, David (2000) Pegasus® Wing-Glove Experiment to Document Hypersonic Crossflow Transition—Measurement System and Selected Flight Results. Technical Report NASA/TM-2000-209016, Research Engineering, NASA Dryden Flight Research Center.
Authors, Various (1984) Peripheral Vision Horizon Display (PVHD). Technical Report NASA Conference Publication CP-2306, Research Engineering, NASA Dryden Flight Research Center.
Bogue, Rodney K. and Erbland, Peter (1993) Perspective on the National Aero-Space Plane Program Instrumentation Development. Technical Report NASA TM-4505, Research Engineering, NASA Dryden Flight Research Center.
Borek, Robert W. (1981) Practical Aspects of Instrumentation Installation in Support of Subsystem Testing, AGARD-CP-299, Paper No. 27, Research Engineering, NASA Dryden Flight Research Center.
Borek, R. W. (1981) Practical Aspects of Instrumentation System Installation, Technical Report AGARD-AG-160-VOL.13, Research Engineering, NASA Dryden Flight Research Center.
Rezek, Terrence W. (1983) Preliminary Experience With a Stereoscopic Video System in a Remotely Piloted Aircraft Application. Technical Report NASA TM-84909, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Moes, Timothy R. and Larson, Terry J. (1990) Preliminary Results From a Subsonic High Angle-of-Attack Flush Airdata Sensing (HI-FADS) System: Design, Calibration, and Flight Test Evaluation. Technical Report NASA TM-101713, Research Engineering, NASA Dryden Flight Research Center.
Moes, Timothy R. and Whitmore, Stephen A. (1991) Preliminary Results From an Airdata Enhancement Algorithm With Application to High-Angle-of-Attack Flight. Technical Report NASA TM-101737, Research Engineering, NASA Dryden Flight Research Center.
Harney, Paul F. (1982) Real-Time Data Display for AFTI/F-16 Flight Testing. Technical Report NASA/TM-1982-84899, Research and Engineering, NASA Dryden Flight Research Center.
Meyer Jr., Robert R. and Schneider, Edward T. (1984) Real-Time Pilot Guidance System for Improved Flight Test Maneuvers. Technical Report NASA TM-84922, Research Engineering, NASA Dryden Flight Research Center.
Bogue, Rodney K. (1993) Recent Flight-Test Results of Optical Airdata Techniques. Technical Report NASA TM-4504, Research Engineering, NASA Dryden Flight Research Center.
Harney, Paul F. and Craft Jr., James B. and Johnson, Richard G. (1985) Remote Control of an Impact Demonstration Vehicle. Technical Report NASA TM-85925, 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 and Engineering, NASA Dryden Flight Research Center.
Borek, Robert W. (1981) Some Practical Aspects of Minimizing the Weight and Volume of Airborne Instrumentation Systems. Meeting Paper AGARD, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Stillwell, Wendell H. and Armistead, Katharine H. (1957) Static-Pressure Error Calibrations for Nose-Boom Airspeed Installations of 17 Airplanes. Technical Report NACA RM H57A02, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Siemers III, Paul M. (1981) Subsonic Tests of an All-Flush-Pressure-Orifice Air Data System. Technical Report NASA TP-1871, Research Engineering, NASA Dryden Flight Research Center.
Chiles, Harry R. (1988) The Design and Use of a Temperature-Compensated Hot-Film Anemometer System for Boundary-Layer Flow Transition Detection on Supersonic Aircraft. Technical Report NASA TM-100421, Research Engineering, NASA Dryden Flight Research Center.
Bever, Glenn A. (1992) The Development of an Airborne Information Management System for Flight Test. Technical Report NASA TM-104251, Research Engineering, NASA Dryden Flight Research Center.
Bever, Glenn A. (1984) The Development of an Airborne Instrumentation Computer System for Flight Test. Technical Report NASA TM-86036, Research Engineering, NASA Dryden Flight Research Center.
Whitmore, Stephen A. and Moes, Timothy R. (1991) The Effects of Pressure Sensor Acoustics on Airdata Derived From a High-Angle-of-Attack Flush Airdata Sensing (HI-FADS) System. Technical Report NASA TM-101736, Research Engineering, NASA Dryden Flight Research Center.
Baumann, Ethan and Pahle, Joseph W. and Davis, Mark C. and White, John Terry (2008) The X-43A Flush Airdata Sensing System Flight Test Results. Meeting Paper AIAA-2008-6570, Research and Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Siemers III, Paul M. (1980) Use of Nose Cap and Fuselage Pressure Orifices for Determination of Air Data for Space Shuttle Orbiter Below Supersonic Speeds. Technical Report NASA TP-1643, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Flechner, Stuart G. and Siemers III, Paul M. (1980) Wind Tunnel Investigation of an All Flush Orifice Air Data System for a Large Subsonic Aircraft. Technical Report NASA TP-1642, Research Engineering, NASA Dryden Flight Research Center.
Larson, Terry J. and Moes, Timothy R. and Siemers III, Paul M. (1990) Wind-Tunnel Investigation of a Flush Airdata System at Mach Numbers From 0.7 to 1.4. Technical Report NASA TM-101697, Research Engineering, NASA Dryden Flight Research Center.
This list was generated on Mon Nov 23 18:15:24 PST 2009.
