Airplane Stability and Control, Second Edition: A History of the Technologies That Made Aviation Possible
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[1] Dong-Chan Lee,et al. Angular Momentum Control in Nonlinear Flight , 2000 .
[2] Lars E. Ericsson. Slender wing rock revisited , 1993 .
[3] Duane T. McRuer,et al. Literal singular-value-based flight control system design techniques , 1989 .
[4] Ronald A. Hess. Methodology for the Analytical Assessment of Aircraft Handling Qualities , 1990 .
[5] Michael Heller,et al. F/A-18E/F Super Hornet high-angle-of-attack control law development and testing , 2001 .
[6] M. V. Cook. On the design of command and stability augmentation systems for advanced technology aeroplanes , 1999 .
[7] Ralph H. Upson. New Developments in Simplified Control , 1942 .
[8] Stephen Osder,et al. Practical View of Redundancy Management Application and Theory , 1999 .
[9] K. G. Johnson,et al. Prediction of Jump Phenomena in Aircraft Maneuvers, including Nonlinear Aerodynamic Effects , 1978 .
[10] Detlef Rohlf,et al. X-31A System Identification Using Single-Surface Excitation at High Angles of Attack. , 1996 .
[11] Long P. Yip,et al. Model flight tests of a spin-resistant trainer configuration , 1992 .
[12] C. D. Perkins. Development of airplane stability and control technology /1970 Von Karman Lecture/ , 1970 .
[13] R. A. Hess,et al. Accommodating a Class of Actuator Failures in Flight Control Systems , 2000 .
[14] David K. Schmidt,et al. Truncation and residualization with weighted balanced coordinates , 1994 .
[15] Richard Whitbeck. A frequency domain approach to linear optimal control. , 1968 .
[16] John J. Burken,et al. Flight-Test Results of Propulsion-Only Emergency Control System on MD-11 Airplane , 1997 .
[17] W. A. Johnson,et al. Study of Control System Effectiveness in Alleviating Vortex Wake Upsets , 1974 .
[18] Robert K. Heffley,et al. Factors Governing Control in a STOL Landing Approach , 1973 .
[19] W. F. Phillips,et al. Improved Closed-Form Approximation for Dutch Roll , 2000 .
[20] J. Steger,et al. Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow , 1980 .
[21] R. Whitbeck,et al. Digital Control Law Synthesis in the w' Domain , 1978 .
[22] R. D. Milne,et al. Some remarks on the dynamics of deformable bodies. , 1968 .
[23] W. H. Phillips,et al. Effects of model scale on flight characteristics and design parameters , 1994 .
[24] R H Hoh,et al. HANDLING QUALITY CRITERION FOR HEADING CONTROL , 1977 .
[25] William H. Philiips. Flying qualities from early airplanes to the Space Shuttle , 1989 .
[26] William Bihrle,et al. Influence of Wing, Fuselage, and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift , 1981 .
[27] W. Bihrle,et al. Spin prediction techniques , 1980 .
[28] George S. Schairer. Directional Stability and Vertical Surface Stalling , 1941 .
[29] D. Mclean. AIRCRAFT FLIGHT CONTROL SYSTEMS , 1999 .
[30] William Bollay. A Theory for Rectangular Wings of Small Aspect Ratio , 1937 .
[31] Duane T. McRuer,et al. Retrospective essay on nonlinearities in aircraft flight control , 1991 .
[32] A. W. Bloy,et al. Directional stability of a large receiver aircraft in air-to-air refueling , 1995 .
[33] Robert F. Stengel. Effect of combined roll rate and sideslip angle on aircraft flight stability , 1975 .
[34] Nelson Pedreiro,et al. Roll-yaw control at high angle of attack by forebody tangential blowing , 1996 .
[35] R. K. Mueller. The Graphical Solution of Stability Problems , 1937 .
[36] Lars E. Ericsson,et al. Conceptual Fluid/Motion Coupling in the Herbst Supermaneuver , 1997 .
[37] Harold Luskin,et al. An Analytical Approach to the Fuel Sloshing and Buffeting Problems of Aircraft , 1952 .
[38] Valerie J. Gawron,et al. When In-Flight Simulation is Necessary , 1995 .
[39] Robert F. Stengel. Altitude stability in supersonic cruising flight , 1970 .
[40] L. E. Root. Empennage Design with Single and Multiple Vertical Surfaces , 1939 .
[41] M. G. Nagati,et al. Multipoint approach for aerodynamic modeling in complex flowfields , 1994 .
[42] William Bollay,et al. Aerodynamic Stability and Automatic Control: The Fourteenth Wright Brothers Lecture , 1951 .
[43] A. Laub,et al. Feedback properties of multivariable systems: The role and use of the return difference matrix , 1981 .
[44] R. H. Hoh,et al. Influence of roll command augmentation systems on flying qualities of fighter aircraft , 1984 .
[45] G. Stein,et al. Multivariable feedback design: Concepts for a classical/modern synthesis , 1981 .
[46] Roland J. White. Investigation of Lateral Dynamic Stability in the XB-47 Airplane , 1950 .
[47] Leo J. Mueller. Pilot and aircraft augmentation on the C-5 , 1970 .
[48] W. P. Rodden,et al. Equations of motion of a quasisteady flight vehicle utilizing restrained static aeroelastic characteristics , 1985 .
[49] Malcolm J. Abzug,et al. Applications of Matrix Operators to the Kinematics of Airplane Motion , 1956 .
[50] F. A. Cleveland,et al. Size effects in conventional aircraft design , 1970 .
[51] C. C. Jahnke,et al. Application of Bifurcation Theory to the High-Angle-of-Attack Dynamics of the F-14 , 1994 .
[52] W. J. Thayer,et al. A Brief History of Electrohydraulic Servomechanisms , 1978 .
[53] Jin Jiang,et al. Design of Reliable Control Systems Possessing Actuator Redundancies , 2000 .
[54] Robert F. Stengel,et al. Effects of displacement and rate saturation on the control of statically unstable aircraft , 1981 .
[55] R. V. Jategaonkar,et al. Evolution of flight vehicle system identification , 1996 .
[56] Robert F. Stengel,et al. Design and flight test of a lateral-directional command augmentationsystem , 1984 .
[57] Joseph Katz,et al. Self-induced roll oscillations of low-aspect-ratio rectangular wings , 1990 .
[58] David K. Schmidt,et al. Modeling and Simulation of Flexible Flight Vehicles , 2001 .
[59] Robert F. Stengel,et al. Jet Transport Response to a Horizontal Wind Vortex , 1995 .
[60] David G. Mitchell,et al. Low-Order Approaches to High-Order Systems: Problems and Promises , 1982 .
[61] H. S. Ribner,et al. Spectral Theory of Buffeting and Gust Response: Unification and Extension , 1956 .
[62] David K. Schmidt,et al. Pilot-vehicle analysis of multiaxis tasks , 1990 .
[63] Donald E. Johnston,et al. Nonsymmetric Flight Influence on High-Angle-of-Attack Handling and Departure , 1976 .
[64] S. Pradeep,et al. Phugoid Approximation Revisited , 1999 .
[65] Duane T. McRuer. Development of pilot-in-the-loop analysis. , 1973 .
[66] Martin E. Beyers. Interpretation of experimental high-alpha aerodynamics. Implications for flight prediction , 1995 .
[67] S. E. Belsley. Man-Machine System Simulation for Flight Vehicles , 1963 .
[68] Robert F. Stengel,et al. Prediction of Pilot-Aircraft Stability Boundaries and Performance Contours , 1978, IEEE Transactions on Systems, Man, and Cybernetics.
[69] William P. Rodden,et al. Structural Dynamics and Quasistatic Aeroelastic Equations of Motion , 2000 .
[70] Gottfried Sachs. Effect of thrust/speed dependence on long-period dynamics in supersonic flight , 1990 .
[71] J. E. Glenn. Manual Flight Control System Functional Characteristics , 1963 .
[72] Isaac Kaminer,et al. Development of Closed-Loop Tail-Sizing Criteria for a High Speed Civil Transport , 1997 .
[73] Clark B. Millikan. The Influence of Running Propellers on Airplane Characteristics , 1940 .
[74] Keun-Shik Chang,et al. Parametric Study of Transient Spoiler Aerodynamics with Two-Equation Turbulence Models , 2001 .
[75] K. W. Iliff,et al. Parameter Estimation for Flight Vehicles , 1989 .
[76] Frederick H. Lutze,et al. Unified development of lateral-directional departure criteria , 1996 .
[77] Malcolm J. Abzug,et al. Effects of Certain Steady Motions on Small-Disturbance Airplane Dynamics , 1954 .
[78] S. I. Pai,et al. Some Aeroelastic Properties of Swept Wings , 1949 .
[79] David L. Kleinman,et al. An optimal control model of human response part I: Theory and validation , 1970 .
[80] V. Mukhopadhyay,et al. A multiloop system stability margin study using matrix singular values. [for wing flutter suppression and drone lateral attitude control] , 1984 .
[81] A. J. Steer,et al. Control and handling qualities considerations for an advanced supersonic transport aircraft , 1999 .
[82] M. V. Cook. The theory of the longitudinal static stability of the hang-glider , 1994 .
[83] Ordway B. Gates. Note on a Criterion for Severity of Roll-Induced Instability , 1959 .
[84] Robert T. Britt,et al. Aeroservoelastic Analysis of the B-2 Bomber , 2000 .
[85] Hans C. Vetter,et al. Effect of a Turbojet Engine on the Dynamic Stability of an Aircraft , 1953 .
[86] Malcolm J. Abzug. Directional Stability and Control During Landing Rollout , 1999 .
[87] A. V. Stephens,et al. Some British Contributions to Aerodynamics , 1966, The Journal of the Royal Aeronautical Society.
[88] Uy-Loi Ly,et al. Stability augmentation design of a large flexible transport using nonlinear parameter optimization , 1996 .
[89] R. Koehler. UNIFIED APPROACH FOR ROLL RATCHETING ANALYSIS , 1999 .
[90] Dietrich Küchemann,et al. Sidney Barrington Gates, 1893-1973 , 1974, Biographical Memoirs of Fellows of the Royal Society.
[91] L. B. Schiff,et al. Directional control at high angles of attack using blowing through a chined forebody , 1995 .
[92] Robert F. Stengel,et al. Stability and Control of Maneuvering High-Performance Aircraft , 1977 .
[93] Marc J. M. Mulkens,et al. Measurements of Aerodynamic Rotary Stability Derivatives Using a Whirling Arm Facility , 1993 .
[94] John N. Perkins,et al. Tailoring stall characteristics using leading-edge droop modifications , 1994 .
[95] Robert F. Stengel,et al. Longitudinal Flying Qualities Criteria for Single-Pilot Instrument Flight Operations , 1983 .
[96] Robert F. Stengel,et al. Toward intelligent flight control , 1993, IEEE Trans. Syst. Man Cybern..