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28 reports
Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part I. The Theory Of control Of Magnetic Amplifier
Author(s): Barker, Richard Clark Corporate Author: Yale Univesity Laboratory: Flight Control Laboratory Date of Publication: 1955-06 Report Number: WADC TR 56-199 Part 1
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The Effects Of Engine Angular Momentum On An Airplane's Longitudinal And Lateral-Directional Dynamic Stability
Author(s): Paiewonsky, Bernard H. Corporate Author: Flight Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1956-06 Report Number: WADC TR 56-225
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Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part V. Summary And Recommendations
Author(s): Barker, Richard Clark Corporate Author: Yale University Laboratory: Flight Control Laboratory Date of Publication: 1956-12 Report Number: WADC TR 56-199 Part 5
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Methods for the Control of Satellites and Space Vehicles: Volume I - Sensing and Actuating Methods
Author(s): Roberson, Robert E. Corporate Author: Systems Corporation of America Laboratory: Flight Control Laboratory Date of Publication: 1960-07-31 Report Number: WADD TR 60-643 Volume 1
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Methods For The Control Of Satellites And Space Vehicles. Volume II. Control System Mechanization And Analysis
Author(s): Roberson, Robert E. Corporate Author: System Corporation Of America Laboratory: Flight Control Laboratory Date of Publication: 1960-07 Report Number: WADD TR 60-643 Volume 2
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Research and Development of a Hot Gas Flight Stabilization System
Author(s): Eclipse- Pioneer Div., Bendix Aviation Corp. Corporate Author: Eclipse-pioneer Div. Bendix Aviation Corporation Laboratory: Flight Control Laboratory Date of Publication: 1960-09 Report Number: WADD TR 60-449 Part I Volume I
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Thermal Effects On Static Aeroelastic Stability And Control. Description and Results of Tests Conducted to Determine the Thermally Affected Deflectional Behavior of Corrugated Multiweb Wing Structures
Author(s): Quinn, James F. Corporate Author: Fligth Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1959-11 Report Number: WADD TR 60-229
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Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part III. The Coordinated Design Of Magnetic Amplifiers And Motors
Author(s): Perrins, Allen R. Corporate Author: Yale University Laboratory: Flight Control Laboratory Date of Publication: 1956-05 Report Number: WADC TR 56-199 Part 3
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Simulation Study Of Control Of An Aircraft At Or Near The Absolute Ceiling
Author(s): Robinson, Alfred C. Corporate Author: Flight Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1956-03 Report Number: WADC TR 56-39
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A Development of the Longitudinal Dynamic Equations of Motion of an Aircraft at the Absolute Ceiling
Author(s): Robinson, Alfred C. Corporate Author: Flight Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1955-05 Report Number: WADC TR 55-210
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Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part II. Superimposed Magnetization In Materials With Rectangular Hysteresis Loops
Author(s): Wakeman, Charles B. Corporate Author: Yale University Laboratory: Flight Control Laboratory Date of Publication: 1955-06 Report Number: WADC TR 56-199 Part 2
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Handbook Of Instructions For Experimentally Determining The Moments Of Inertia And Product O Finertia Of Aircraft By The Spring Oscillation Method
Author(s): Woodward, Claude R. Corporate Author: Cornell Aeronautical Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1955-06 Report Number: WADC TR 55-415
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The Air Force Integrated Flight Instrument Panel
Author(s): Svimonoff, Constantine Corporate Author: Flight Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1958-10 Report Number: WADC TR 58-431
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Study And Development Of Magnetic Amplifier Controlled Servo Systems. Part IV. Diverse Topics: Magnetic Frequency Multipliers, Two Phase Servo, Relay Servo, Input Circuits, Coupling Networks
Author(s): Barker, R. C. Corporate Author: Yale University Laboratory: Flight Control Laboratory Date of Publication: 1956-09 Report Number: WADC TR 56-199 Part 4
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The Air Force Program For Improved Flight Instrumentation
Author(s): Wright, Lawrence C. Corporate Author: Flight Control Laboratory Laboratory: Flight Control Laboratory Date of Publication: 1956-11 Report Number: WADC TR 56-582
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The Determination Of Lateral Handling Quality Requirements From Airframe-Human Pilot System Studies
Author(s): Ashkenas, Irving L. Corporate Author: Systems Technology, Inc. Laboratory: Flight Control Laboratory Date of Publication: 1959-06 Report Number: WADC TR 59-135
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Altimeter Display and Hardware Development 1903-1960
Author(s): Schum, David A. Corporate Author: Bell Helicopter Company Laboratory: Flight Control Laboratory Date of Publication: 1963-05 Report Number: ASD TDR 63-288
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Summary Of Component Failure Rate And weighting Function Data And Their Use In Systems Preliminary Design
Author(s): Johnston, Donald E. Corporate Author: Control Specialists Division, Kelsey-Hayes Laboratory: Flight Control Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-668
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Human Pilot Dynamic Response In Flight And Simulator
Author(s): Seckel, Edward Corporate Author: James Forrestal Research Center, Princeton University Laboratory: Flight Control Laboratory Date of Publication: 1958-08 Report Number: WADC TR 57-520
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Methods For Estimating Aeroelastic Effects On Subsonic Lateral-directional Stability Derivitives Of Aircraft
Author(s): Cahen, George L. Corporate Author: Glenn L. Martin Company Laboratory: Flight Control Laboratory Date of Publication: 1956-10 Report Number: WADC TR 56-345
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Study To Determine An Automatic Flight Control Configuration To Provide A Stability Augmentation Capability For High Performance Supersonic Aircraft
Author(s): Van Meter, J. T. Corporate Author: Minneapolis-Honeywell Regulator Company Laboratory: Flight Control Laboratory Date of Publication: 1957-06 Report Number: WADC TR 57-349
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An Analytical Study Of The Dynamics Of Spinning Aircraft. Part 2. Wind Tunnel Tests
Author(s): Wykes, John H. Corporate Author: North American Aviation, Inc. Laboratory: Flight Control Laboratory Date of Publication: 1958-12 Report Number: WADC TR 58-381 Part 2
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An Analytical Study Of The Dynamics Of Spinning Aircraft. Part 1. Flight Test Data Analyses And Spin Claculations
Author(s): Wykes, John H. Corporate Author: North American Aviation, Inc. Laboratory: Flight Control Laboratory Date of Publication: 1958-12 Report Number: WADC TR 58-381 Part 1
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Boundary Layer Control Applied To Tail Surfaces Of Aircraft . Part I: Wind Tunnel Report
Author(s): Leisher, L. L. Corporate Author: Cessna Aircraft Company Laboratory: Flight Control Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-741 Part 1
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Magnetic Servo Amplifliers For Flight Control Systems
Author(s): Frank, Max Corporate Author: Wayne Engineering Research Institute, Wayne University Laboratory: Flight Control Laboratory Date of Publication: 1956-10 Report Number: WADC TR 56-271
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The Effects Of Structural Elasticity On Aircraft Control Systems
Author(s): Howard, Vincent W. Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology Laboratory: Flight Control Laboratory Date of Publication: 1956-06 Report Number: WADC TR 56-166
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Boundary Layer Control Applied To Tail Surfaces Of A Aircraft . Part II: Final Report
Author(s): Gersten, W. M. Corporate Author: Cessna Aircraft Company Laboratory: Flight Control Laboratory Date of Publication: 1957-12 Report Number: WADC TR 57-741 Part 2
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A Study Of Angle-of-attack Angle-of-sideslip Pitot-static Probes
Author(s): Smetana, Frederick O. Corporate Author: University Of Southern California Laboratory: Flight Control Laboratory Date of Publication: 1958-01 Report Number: WADC TR 57-234
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