References and Core BibliographyChapter 1. Early Developments in Stability and ControlBryan, George H. 1911. Stability in Aviation. London: MacMillan
Gibson, John C. 2000. Unpublished comments on the first edition of Airplane Stability and Control, Cambridge U. Press, 1997
Jex, Henry R., and Fred. E. C. Culick 1985. Flight Control Dynamics of the 1903 Wright Flyer, Proc. of the 12th Atmospheric Flight Control Conf., New York: AIAA, pp. 534–548
Jones, B. Melvill 1934. Dynamics of the Airplane, in Aerodynamic Theory, Vol. V, ed. W. F. Durand, Berlin: Springer, pp. 1–222
Lednicer, David 2001. Unpublished comments in letter dated February 2, referring to NACA Report 254 by A. J. Fairbanks on pressure distribution tests of a model of the Fokker D VII
Chapter 2. Teachers and TextsMilliken, William F. Jr. 1947. Progress in Dynamic Stability and Control Research, Jour. of the Aeronautical Sciences, Vol. 14, No. 9, pp. 493–518
Chapter 3. Flying Qualities Becomes a ScienceAnderson, Seth B., Hervey C. Quigley, and Robert C. Innis 1965. Stability and Control Considerations for STOL Aircraft, AGARD Rept. 504
Anon. 1980. Military Specification. Flying Qualities of Piloted Airplanes, MIL-F-8785C
Anon. 1983. Design and Airworthiness Requirements for Service Aircraft. Defense Standard 00-970/Issue 1, Vol. 1, Book 2, Part 6 – Aerodynamics, Flying Qualities and Performance, Ministry of Defense, UK
Anon. 1987. Flying Qualities of Piloted Vehicles, MIL-STD-1797, USAF
Anon. 1994. Joint Aviation Requirements – JAR 25-Large Airplanes, Section 1 – Requirements, Subpart B – Flight, Joint Aviation Authority
Ashkenas, Irving L. et al. 1973. Recommended Revisions to Selected Portions of MIL-F-8785(ASG) and Background Data, AFFDL-TR-73-76
Ashkenas, Irving L. 1985. Collected Flight and Simulation Comparisons and Considerations, in AGARD CP 408. (64 references)
Assadourian, A. and John A. Harper 1953. Determination of the Flying Qualities of the Douglas DC-3 Airplane, NACA TN 3088
Barnes, Arthur G. 1988. The Role of Simulation in Flying Qualities and Flight Control System Related Development, in AGARD LS 157
Belsley, Steven E. 1963. Man-Machine System Simulation for Flight Vehicles, IEEE Transactions on Human Factors in Electronics, Vol. HFE-4, No. 1, pp. 4–14
Bryan, George H. 1911. Stability in Aviation, London: MacMillan
Breuhaus, Waldemar O., 1991. The Variable Stability Airplane, from a Historical Perspective, American Aviation Historical Society Jour., Vol. 36, No. 1, pp. 30–55
Chalk, Charles R., T. P. Neal, T. M. Harris, F. E. Pritchard, and Robert J. Woodcock 1969. Flying Qualities of Piloted Airplanes, Background Information and Users Guide for MIL-F-8785 (ASG), AFFDL-TR-69–72
Cook, M. V. 1994. The Theory of the Longitudinal Static Stability of the Hang Glider, The Aeronautical Jour., Vol. 98, No. 978, pp. 292–304
Cook, M. V. 1997 Flight Dynamics Principles, London: Arnold, pp. 212–214
Cooper, George E. and Robert P. Harper, Jr., 1969. The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities, NASA TN D-5153
Coyle, Shawn 1996. The Art and Science of Flying Helicopters, Ames: Iowa State University Press, pp. 91–92
Craig, Samuel J. and Heffley, Robert K. 1973, Factors Governing Control in a STOL Landing Approach, Jour. of Aircraft, Vol. 10, No. 8, pp. 495–502
Donlan, Charles J. 1944. An Interim Report on the Stability and Control of Tailless Airplanes, NACA Rept. 796
Fielding, C., and Lodge, M. 2000. Stability and Control of STVOL Aircraft: The Design of Longitudinal Flight Control Laws, The Aeronautical Jour., Vol. 104, No. 1038, pp. 383–389
Gawron, V. J. and Reynolds, P. A. 1995. When In-Flight Simulation is Necessary, Jour. Of Aircraft, Vol. 32, No. 2, pp. 441–415
Gilruth, Robert R. and M. D. White 1941. Analysis and Prediction of Longitudinal Stability of Airplanes, NACA Rept. 711
Gilruth, Robert R. and W. N. Turner 1941. Lateral Control Required for Satisfactory Flying Qualities Based on Flight Tests of Numerous Airplanes, NACA Rept. 715
Gilruth, Robert R. 1943. Requirements for Satisfactory Flying Qualities of Airplanes, NACA Rept. 755
Glauert, H. 1934. Airplane Propellers, Divsion L of Aerodynamic Theory, Vol. IV, ed. by W. F. Durand, California, Durand Reprinting Committee, pp. 348–351
Goett, Harry J., Robert P. Jackson, and Steven E. Belsley, 1944. Wind-Tunnel Procedure for Determination of Critical Stability and Control Characteristics of Airplanes, NACA Rept. 781
James, Hansen R. 1987. Engineer in Charge, NASA SP-4305
Harris, D., Gautrey, J., Payne, K., and Bailey, R. 2000. The Cranfield Aircraft Handling Qualities Rating Scale: A Multidimensional Approach to the Assessment of Aircraft Handling Qualities, The Aeronautical Jour., Vol. 104, No. 1034, pp. 191–198
Hoh, Roger H. and M. B. Tischler 1983. Status of the Development of Handling Criteria for VSTOL Transition, AIAA Paper 83-2103
Hoh, Roger, H. 1983. Bring Cohesion to Handling-Qualities Engineering, Astronautics and Aeronautics, June, pp. 64–69
Hoh, Roger H., 1981. Development of Handling Quality Criteria for Aircraft With Independent Control of Six Degrees of Freedom, AFWAL-TR-81-3027
Hoh, Roger H., David G. Mitchell, and Steven R. Sturmer 1987. Handling Qualities Criteria for STOL Landings, STI Paper 407
Kandalaft, R. N. 1971. Validation of the Flying Qualities Requirements of MIL-F-8785B(ASG), AFFDL-TR-71-134
Kayten, Gerald G. 1945. Analysis of Stability and Control in Terms of Flying Qualities of Full-Scale Airplanes, NACA Rept. 825
Mitchell, D. G. and R. H. Hoh 1983. Handling Qualities Criteria for STOL Flight Path Control for Approach and Landing, AIAA Paper 83-2106
Mooij, H. A. 1985. Criteria for Low-Speed Longitudinal Handling Qualities: of Transport Aircraft with Closed-Loop Flight Control Systems. Dordrecht: Martinus Nijhoff Publ
Moorhouse, David J. and Robert J. Woodcock 1982. Military Specification – Flying Qualities of Piloted Airplanes, AFWAL-TR-81-3109. Background Information and User Guide for MIL-F-8785C, (120 references)
Myers, Thomas T., Donald E. Johnston, and Duane T. McRuer 1987. Space Shuttle Flying Qualities and Criteria Assessment, NASA CR 4049
Phillips, William H. 1948. Appreciation and Prediction of Flying Qualities, NACA Rept. 927
Phillips, William H. 1994. Effects of Model Scale on Flight Characteristics and Design Parameters, Jour. of Aircraft, Vol. 31, No. 2, pp. 454–457
Rolfe, J. M. and K. J. Staples (eds.) 1986. Flight Simulation, London: Cambridge U. Press
Shafer, Mary F. 1993. In-Flight Simulation at the NASA Dryden Flight Research Facility, American Aviation Historical Society, Vol. 38, No. 4, pp. 261–277
Shanks, G. T., S. L. Gale, C. Fielding, and D. V. Griffith 1996. Flight Control and Handling Research with the VAAC Harrier Aircraft, in Advances in Aircraft Flight Control, ed. M. B. Tischler, London: Taylor and Francis, pp.159–186
Soulé, Hartley A. 1940. Preliminary Investigation of the Flying Qualities of Airplanes, NACA Rept. 700
Stapleford, R. L., D. T. McRuer, R. H. Hoh, D. E. Johnston, and R. K. Heffley 1970. Outsmarting MIL-F-8785B(ASG), Systems Technology Inc. TR-190-1
Stengel, Robert F. 1979. In-Flight Simulation With Pilot-Center of Gravity Offset and Velocity Mismatch, Jour. of Guidance and Control, Vol. 2, No. 6, pp. 538–540
Stinton, Darrol 1996. Flying Qualities and Flight Testing of the Airplane, Reston, Virginia: AIAA, pp. 5, 6
Thomas, H. H. B. M. and Küchemann, D. 1974. Sidney Barrington Gates 1893–1973, Biog. Memoirs of Fellows of the Royal Soc., Vol. 20, pp. 181–212
Tischler, M. B. and R. H. Hoh 1982. Handling Qualities Criterion for Flight Path Control of V/STOL Aircraft, AIAA Paper 82–1292
Warner, Edward P. and Frederick H. Norton 1970. Preliminary Report on Free Flight Tests, NACA Rept. 70
Westbrook, Charles B. and McRuer, Duane T. 1979. Handling Qualities and Pilot Dynamics, Aero/Space Engineering, Vol. 18, No. 5, pp. 26–32
Woodcock, Robert J. and J. T. Browne 1986. The Mil-Prime Standard for Aircraft Flying Qualities, Proc. of the AIAA Atmospheric Flight Mechanics Conf., New York: AIAA, pp. 232–238
Chapter 4. Power Effects on Stability and ControlGilruth, Robert R. and M. D. White 1941. Analysis and Prediction of Longitudinal Stability of Airplanes, NACA Rept. 711
Goett, Harry J. and Noel Delany 1944. Effect of Tilt of the Propeller Axis on the Longitudinal Stability Characteristics of Single-Engine Airplanes, NACA Rept. 774
Lee, John G. 1984. It Should Fly Wednesday. Connecticut: Mystic Publications, Inc
McKinney, Marion O., Jr., Richard E. Kuhn, and John P. Reeder 1964. Aerodynamics and Flying Qualities of Jet V/STOL Airplanes, SAE Paper 864A
Millikan, Clark B. 1940. The Influence of Running Propellers on Airplane Characteristics, Jour. of the Aeronautical Sciences, Vol. 7, No. 3, pp. 85–103
Phillips, William H., H. L. Crane, and Paul A. Hunter 1944. Effect of Lateral Shift of the Center of Gravity on Rudder Deflection Required for Trim, NACA WR L-92
Relf, E. F. 1922. An Electric Motor of Small Diameter for Use Inside Aeroplane Models, British R & M 778
Ribner, Herbert S. 1944. Notes on the Propeller and Slipstream in Relation to Stability, NACA WR L-25
Ribner, Herbert S. 1945. Formulas for Propellers in Yaw and Charts of the Side-Force Derivative, NACA Rept. 819
Ribner, Herbert S. 1945. Propellers in Yaw, NACA Rept. 820
Ribner, Herbert S. 1946. Field of Flow About a Jet and Effect of Jets on Stability of Jet-Propelled Airplanes, NACA ACR L6C13
Smelt, Ronald and H. Davies 1937. Estimation of Increase in Lift Due to Slipstream, British R & M 1788
Squire, H. B. and J. Trouncer 1944. Round Jets in a General Stream, British R & M 1974
Vetter, Hans C. 1953. Effect of a Turbojet Engine on the Dynamic Stability of an Aircraft, Jour. of the Aeronautical Sciences, Vol. 20, No.11, pp. 797, 798
Chapter 5. Managing Control ForcesAmes, Milton B., Jr. and Richard I. Sears 1941. Determination of Control-Surface Characteristics from NACA Plain-Flap and Tab Data, NACA Rept. 721
Baumgarten, G. and W. Heine 1996. A New Reconfiguration Concept for Flight Control Systems in Case of Actuator and Control Surface Failures. Proc. of the 20thCongress of the ICAS, Sorrento, Italy, Sept 8–13, 1996
Brown, W. S. 1941. Spring Tab Controls, British R & M 1979
Bryant, L. W. and R. W. G. Gandy 1939. An Investigation of the Lateral Stability of Aeroplanes with Rudder Free, NPL Rept. S&C 1097
Bureau of Aeronautics 1953. The Hydraulics System, Rept. AE-61-4 IV
Chambers, Joseph R. 2000. Partners in Freedom, Monographs in Aerospace History No. 19, NASA SP-2000-4519, pp. 154, 155
Choi, Seong-Wook, Chang, Keun-Shik, and Ok, Honam 2001. Parametric Study of Transient Spoiler Aerodynamics with Two-Equation Turbulence Models, Jour. of Aircraft, Vol. 38, No. 5, pp. 888–894
Dunn, Orville R. 1949. Aerodynamically Boosted Surface Controls and Their Application to the DC-6 Transport, I.A.S.-R.Ae. S. Proc., pp. 503–533
Gates, Sidney B. 1940. Note on Differential Gearing as a Means of Aileron Balance, British R & M 2526
Gates, Sidney B. 1941. Notes on the Spring Tab, Rept. B.A. 1665, British R.A.E.
Glauert, Hermann 1927. The Theoretical Relationships for an Aerofoil With Hinged Flap, British R & M 1095
Glenn, John E. 1963. Manual Flight Control System Functional Characteristics, IEEE Transactions on Human Factors in Electronics, Vol HFE-4, No. 1, pp. 29–38
Goranson, R. Fabian 1945. Flight Tests of Experimental Beveled Trailing Edge Frise Ailerons on a Fighter Airplane, NACA TN 1085
Gough, Melvin N. and A. P. Beard 1936. Limitations of the Pilot in Applying Forces to Airplane Controls, NACA TN 550
Graham, Dunstan and McRuer, Duane T. 1991. Retrospective Essay on Nonlinearities in Aircraft Flight Control, Jour. of Guidance, Control, and Dynamics, Vol. 14, No. 6, pp. 1089–1099
Greenberg, Harry and Leonard Sternfield 1943. A Theoretical Investigation of the Lateral Oscillations of an Airplane with Free Rudder with Special Reference to the Effect of Friction, NACA Rept. 762
Greenberg, Harry 1944. Calculation of Stick Forces for an Elevator with a Spring Tab, NACA WR L-139
Harschburger, H. E. 1983. Development of Redundant Flight Control Actuation Systems for the F/A-18 Strike Fighter, SAE Paper 831484
Hess, R. A., Siwakosit, W., and Chung, J. 2000. Accommodating a Class of Actuator Failures in Flight Control Systems, Jour. of Guidance, Control, and Dynamics, Vol. 23, No. 3, pp. 412–419
Howard, R. W. 2000. Planning for Super Safety: The Fail-Safe Dimension, The Aeronautical Jour., Vol. 104, No. 1041, pp. 517–555
Jiang, Jin and Zhao, Qing 2000. Design of Reliable Control Systems Possessing Actuator Redundancies, Jour. of Guidance, Control, and Dynamics, Vol. 23, No. 4, pp. 709–718
Jones, Robert T. and Albert I. Nerkin 1936. The Reduction of Aileron Operating Force by Differential Linkage, NACA TN 586
Jones, Robert T. and Doris Cohen 1941. An Analysis of the Stability of an Airplane with Free Controls, NACA Rept. 709
Jones, Robert T. and Milton B. Ames 1942. Wind Tunnel Investigation of Control-Surface Characteristics. V. – The Use of a Beveled Trailing Edge to Reduce the Hinge Moment of a Control Surface, NACA ARR
Jones, Robert T. and Harold F. Kleckner 1943. Theory and Preliminary Flight Tests of an All-Movable Vertical Tail Surface, NACA WR L-496
Lyle, Bruce S. 1983. Development of Control Surface Actuation Systems on Various Configurations of the F-16, SAE Paper 831483
Maskrey, Robert H. and Thayer, W. J. 1978. A Brief History of Electrohydraulic Servomechanisms, Jour. of Dynamic Systems, Measurement and Control (ASME), Vol. 100, No. 2, pp. 110–116
Mathews, Charles W. 1944 An Analytical Investigation of the Effect of Elevator Fabric Distortion on the Longitudinal Stability and Control of an Airplane, NACA ACR L4E30
McAvoy, William H. 1937. Maximum Forces Applied by Pilots to Wheel-Type Controls, NACA TN 623
McLean, D. 1999. Aircraft Flight Control Systems, The Aeronautical Jour., Vol. 103, No. 1021, pp. 159–165
McMahan, Jack 1983. Appendix A of Restructurable Controls, NASA CP 2277
MrRuer, Duane T. (chair) 1997. Report of the Committee on the Effects of Aircraft-Pilot Coupling on Flight Safety, Washington, DC: National Academy Press, pp. 26, 55–73
Osder, Stephen 1999. Practical View of Redundancy Management – Application and Theory, Jour. Of Guidance, Control, and Dynamics, Vol. 22, No. 1, pp. 12–21
Perrin, W. G. 1928. The Theoretical Relationships for an Aerofoil With a Multiply Hinged Flap System, British R & M 1171
Phillips, William H., B. P. Brown, and J. L. Matthews, Jr. 1953. Review and Investigation of Unsatisfactory Control Characteristics Involving Instability of Pilot-Airplane Combination and Methods of Predicting These Difficulties From Ground Tests, NACA RM L53F17a
Phillips, William H. 1944. Application of Spring Tabs to Elevator Controls, NACA Rept. 797
Rogallo, Francis M. 1944. Collection of Balanced Aileron Test Data, NACA WR (ACR) 4A11
Root, L. Eugene 1939. Empennage Design with Single and Multiple Vertical Surfaces”, Jour. of the Aeronautical Sciences, Vol. 6, No. 9, pp. 353–360
Schaefer, W. S., L. J. Inderhees, and John F. Moynes 1991. Flight Control Actuation System for the B-2 Advanced Technology Bomber, Proc. of the SAE Aerospace Atlantic Conf. SAE Paper 911112, 14pp
Schmitt, Vernon R., James W. Morris, and Gavin D. Jenney 1998. Fly-By-Wire – A Historical and Design Perspective, SAE IBSN 0-7680-0218-4
Sears, William R. 1987 (July) Flying Wing Could Stealthily Reappear, Aerospace America, Vol. 25, No. 7, pp. 16–19
Silverstein, Abe and S. Katzoff 1940. Aerodynamic Characteristics of Horizontal Tail Surfaces, NACA Rept. 688
Toll, Thomas A. 1947. A Summary of Lateral Control Research, NACA Rept. 868
Tomayko, James E. 2000. Computers Take Flight: A History of NASA's Pioneering Digital Fly-by-Wire Project, NASA SP-200-4224
Waterman, A. W. 1983, The Boeing 767 Hydraulic System, SAE Paper 831488
Weick, Fred C. 1987. From the Ground Up, Washington: Smithsonian Inst
White, Roland J. 1950. Investigation of Lateral Dynamic Stability in the XB-47 Airplane, Jour. of the Aeronautical Sciences, Vol. 17, No. 3, pp. 133–148
Chapter 6. Stability and Control at the Design StageAbbott, Ira H., A. E. Von Doenhoff, and L. S. Stivers, Jr. 1945. Summary of Airfoil Data, NACA Rept. 824
Campbell, John P. and Marion O. McKinney 1952. Summary of Methods for Calculating Dynamic Lateral Stability and Response and for Estimating Lateral Stability Derivatives, NACA Rept. 1098
Anon 1974. Royal Aeronautical Society (RAeS) Data Sheets, Engineering Sciences Data Item No. 74011, Aerodynamics Sub-series
Bloy, A. W. and Lea, K. A. 1995. Directional Stability of a Large Receiver Aircraft in Air-to-Air Refueling, Jour. of Aircraft, Vol. 32, No. 2, pp. 453–455
DeYoung, John 1948. Theoretical Symmetric Span Loading at Subsonic Speeds for Wings Having Arbitrary Plan Form, NACA Rept. 921
DeYoung, John 1951. Theoretical Antisymmetric Span Loading for Wings of Arbitrary Plan Form at Subsonic Speeds, NACA Rept. 1056
DeYoung, John 1952. Theoretical Symmetric Span Loading due to Flap Deflection for Wings of Arbitrary Plan Form at Subsonic Speeds, NACA Rept. 1071
De Young, John 1976. Vortex Lattice Utilization, NASA SP-405
Diederich, Franklin W. 1951. Charts and Tables for use in Calculations of Downwash of Wings of Arbitrary Plan Form, NACA TN 2353
Falkner, V. M. 1943. The Calculation of Aerodynamic Loading on Surfaces of any Shape, British A.R.C.R. and M. No. 1910
Hoak, Donald E. et al. 1976 (rev.). USAF Stability and Control DATCOM, U.S. Air Force Flight Dynamics Lab
House, Rufus O. and Arthur R. Wallace 1941. Wind-Tunnel Investigation of Effect of Interference on Lateral-Stability Characteristics of Four NACA 23012 Wings, an Elliptical and Circular Fuselage, and Vertical Fins, NACA Rept. 705
Jameson, A., W. Schmidt, and E. Turkel 1981. Numerical Solution of the Euler Equation by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes, AIAA Paper 81-1259
Jones, Robert T. 1946. Properties of Low-Aspect Ratio Pointed Wings at Speeds Below and Above the Speed of Sound, NACA Rept. 835
Kaminer, Isaac I., Howard, Richard M., and Buttrill, Carey S. 1997. Development of Closed-Loop Tail-Sizing Criteria for a High Speed Civil Transport, Jour. of Aircraft, Vol. 34, No. 5, pp. 638–664
Kayten, Gerald G. and William Koven 1945. Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas A-26 Airplane, NACA Rept. 816
Multhopp, Hans 1941. Aerodynamics of the Fuselage, NACA TM 1036
Munk, Max M. 1923. The Aerodynamic Forces on Airship Hulls, NACA Rept. 184
Pearson, Henry A. and Robert T. Jones 1938. Theoretical Stability and Control Characteristics of Wings With Various Amounts of Taper and Twist, NACA Rept. 635
Pulliam, T. H. and Steger, J. L. 1989. Implicit Finite Difference Simulations of Three-Dimensional Compressible Flow, AIAA Jour., Vol. 18, No. 2, pp. 159–167
Silverstein, Abe and S. Katzoff 1939. Design Charts for Predicting Downwash Angles and Wake Characteristics behind Plain and Flapped Wings, NACA Rept. 648
Smith, A. M. O. 1962. Incompressible Flow About Bodies of Arbitrary Shape, IAS Paper No. 62–143, presented at the IAS National Sciences Meeting, Los Angeles, CA, June
Chapter 7. The Jets at an Awkward AgeAbzug, M. J. 1956. Application of Matrix Operators to the Kinematics of Airplane Motion, Jour. of the Aeronautical Sciences, Vol. 23, No. 7, pp. 679–684
Gunston, Bill 1973. Bombers of the West, New York: Scribners
Chapter 8. The Discovery of Inertial CouplingAbzug, M. J. 1954. Effects of Certain Steady Motions on Small-Disturbance Airplane Motions, Jour. of the Aeronautical Sciences, Vol. 21, pp. 749–762
Bergrun, Norman and Paul Nickel 1953. A Flight Investigation of the Effect of Steady Rolling on the Natural Frequencies of a Body-Tail Combination, NACA TN 2985
Gates, O. B. and Minka, K. 1959. Note on a Criterion for Severity of Roll-Induced Instability, Jour. of the Aero/Space Sciences, Vol. 26, No. 6, pp. 287–290
Phillips, William H. 1948. Effect of Steady Rolling on Longitudinal and Directional Stability, NACA TN 1627
Phillips, William H. 1992. Recollections of Langley in the Forties, Jour. of the Amer. Aviation Historical Soc., Vol. 37, No. 2, pp. 116–127
Pinsker, W. J. G. 1957. Critical Flight Conditions and Loads Resulting From Inertia Cross-Coupling and Aerodynamic Stability Deficiencies, RAE Tech Note Aero 2502
Belsley, Rhoads D. W. and Schuler, John M. 1957. A Theoretical and Experimental Study of Airplane Dynamics in Large-Disturbance Maneuvers, Jour. of the Aeronautical Sciences, Vol. 24, No. 7, pp. 507–526, 532
Schy, Albert A. and Hannah, M. E. 1977. Prediction of Jump Phenomena in Roll Coupled Maneuvers of Airplanes, Jour. of Aircraft, Vol. 14, pp. 375–382
Seckel, E. 1964. Stability and Control of Airplanes and Helicopters, New York: Academic Press
Stengel, Robert F. 1975. Effect of Combined Roll Rate and Sideslip Angle on Aircraft Flight Stability, Jour. of Aircraft, Vol. 12, No. 8, pp. 683–685
Thomas, H. H. B. M. and P. Price 1960. A Contribution to the Theory of Aircraft Response in Rolling Manoeuvres Including Inertia Cross-Coupling Effects, British R & M 3349
Weil, Joseph and Richard E. Day 1956. An Analog Study of the Relative Importance of Various Factors Affecting Roll Coupling, NACA RM H56A06
Westbrook, Charles B. (ed.) 1956. Transactions of the Wright Air Development Center Conference on Inertia Coupling of Aircraft, 56 WCLC-1041
Young, J. W., Schy, A. A., and Johnson, K. G. 1978. Prediction of Jump Phenomena in Aircraft Maneuvers, Including Nonlinear Aerodynamic Effects, Jour. of Guidance and Control, Vol. 1, No. 1, pp. 26–31
Chapter 9. Spinning and RecoveryAbzug, M. J. 1977. Spin and Recovery Characteristics of the Rockwell Model 680F, ACA Systems Rept. R-143
Adams, W. M. 1972. Analytical Prediction of Airplane Equilibrium Spin Characteristics, NASA TN D-6926
Anderson, Seth B., Enevoldson, Einar K., and Luat T. Nguyen 1983. Pilot Human Factors in Stall/Spin Accidents of Supersonic Fighter Aircraft, in AGARD CP-347
Arena, Andrew S., Jr., R. C. Nelson, and L. B. Schiff 1990. An Experimental Study of the Nonlinear Dynamic Phenomenon Known as Wing Rock, AIAA Paper 90-2812-CP, pp. 173–183
Beaurain, L. 1977. General Study of Light Plane Spin, Aft Fuselage Geometry, Part 1, NASA TTF-17-446
Beyers, Martin E. 1995. Interpretation of Experimemtal High-Alpha Aerodynamics – Implications for Flight Prediction, Jour. of Aircraft, Vol. 32, No. 2, pp. 247–261 (80 references)
Bihrle, William, Jr. 1957. Analytic Investigations of an Unconventional Airplane Spin, in Trans. of the Wright Air Development Center Airplane Spin Symposium, ed. C. B. Westbrook and H. K. Doetsch, 57 WCLC-1688 and -1774
Bihrle, William, Jr., and Billy Barnhart 1978. Design Charts and Boundaries for Identifying Departure Resistant Fighter Configurations, Naval Air Devel. Center Rept. 76154-30
Bihrle, William Jr. 1981. Influence of Wing, Fuselage, and Tail Design on Rotational Flow Aerodynamics Beyond Maximum Lift, Jour. of Aircraft, Vol. 18, No. 11, pp. 920–925
Bihrle, William Jr. and Barnhart, Billy 1983. Spin Prediction Techniques, Jour. of Aircraft, Vol. 20, No. 2, pp. 97–101
Bowman, James S., Jr. 1971. Summary of Spin Technology as Related to Light General Aviation Airplanes, NASA TN D-6575
Bowman, James S., Jr. 1989. Measurements of Pressures on the Tail and Aft Fuselage of an Airplane Model During Rotary Motions at Spin Attitudes, NASA TP-2939
Burk, Sanger M., Jr., James S. Bowman, Jr., and William L. White 1977. Spin-Tunnel Investigation of the Spinning Characteristics of Typical Single-Engine General Aviation Designs. I – Low-Wing Model A: Effects of Tail Configurations, NASA TP-1009
Chambers, Joseph R. and H. Paul Stough III 1986. Summary of NASA Stall/Spin Research for General Aviation Configurations, AIAA Paper 86-2597
Chambers, Joseph R. 2000. Partners in Freedom, Monographs in Aerospace History No. 19, NASA SP-2000-4519, pp. 91–94, 102–105, 223
Ericsson, Lars E. 1993. Slender Wing Rock Revisited, Jour. of Aircraft, Vol. 30, No. 3, pp. 352–356
Gates, Sidney B. and L. W. Bryant 1926. The Spinning of Aeroplanes, British R & M 1001
Belsley, Goman M. and Khrabov, A. 1994. State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack, Jour. of Aircraft, Vol. 31, No. 5, pp. 1109–1115
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Johnston, Donald E. and Hogge, Jeffrey R. 1976. Nonsymmetric Flight Influence on High Angle of Attack Handling and Departure, Jour. of Aircraft, Vol. 13, No. 2, pp. 112–118
Kalviste, Juri 1978. Aircraft Stability Characteristics at High Angles of Attack, in AGARD CP 235
Kalviste, Juri 1982. Use of Rotary Balance and Forced Oscillation Test Data in a Six-Degree-of-Freedom Simulation, AIAA Paper 82-1364
Kalviste, Juri and Bob Eller 1989. Coupled Static and Dynamic Stability Parameters, AIAA Paper 89-3362
Levin, Daniel and Katz, Joseph 1992. Self-Induced Roll Oscillations of Low-Aspect-Ratio Rectangular Wings, Jour. of Aircraft, Vol. 29, No. 4, pp. 698–702
Lee, Dong-Chan and M. G. Nagati 1999. Improved Coupled Force and Moment Parameter Estimation for Aircraft, AIAA Paper 99-4174, in Collection of the AIAA Atmospheric Flight Mechanics Conference Technical Papers, Portland, OR, 9–11 Aug 1999, pp. 484–492
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Lutze, F. H., , W. C. Durham, and Mason, W. H. 1996. Unified Development of Lateral-Directional Departure Criteria, Jour. of Guidance, Control, and Dynamics, Vol. 19, No. 2, pp. 489–493
Mangold, Peter 1991. Transformation of Flightmechanical Design Requirements for Modern Fighters into Aerodynamic Characteristics, in Manoeuvering Aerodynamics, AGARD CP-497
Mitchell, David G. and Donald E. Johnston 1980. Investigation of High-Angle-of-Attack Maneuvering-Limiting Factors, AFWAL-TR-80-3141, Part II
Moul, Martin T. and John W. Paulson 1958. Dynamic Lateral Behavior of High Performance Aircraft, NACA RM L58E16
Neihouse, Anshal I., Jacob H. Lichtenstein, and Philip W. Pepoon 1946. Tail Design Requirements for Satisfactory Spin Recovery, NACA TN 1045
Neihouse, Anshal I., Walter J. Klinar, and Stanley H. Sher 1960. Status of Spin Research for Recent Airplane Designs, NASA R-57
Nelson, R. C. and A. S. Arena, Jr. 1992. An Experimental Investigation of Wing Rock of Slender Wings and Airplane Configurations, Proc. of the Fluid Dynamics at High Angles of Attack Conference, Tokyo
Pinsker, W. J. G. 1967. Directional Stability in Flight with Bank Angle Constraint as a Condition Defining a Minimum Acceptable Value for nv, RAE Technical Report 67-127
Polhamus, Edward C. 1966. A Concept of the Vortex Lift of Sharp-Edge Delta Wings Based on a Leading Edge Suction Analogy, NASA TN D-3767
Relf, E. F. and T. Lavemder 1918. Auto-Rotation of Stalled Aerofoils and its relation to the Spinning Speed of Aeroplanes, British R & M 549
Relf, E. F. and T. Lavender 1922, 1925. British R & M's 828 and 936
Ross, A. Jean and Luat T. Nguyen 1988. Some Observations Regarding Wing Rock Oscillations at High Angles of Attack, AIAA Paper 88-4371-CP
Ross, Holly M. and Perkins, John N. 1994. Tailoring Stall Characteristics Using Leading-Edge Droop Modifications, Jour. of Aircraft, Vol. 31, No. 4, p. 767
Scher, Stanley H. 1954. An Analytical Investigation of Airplane Spin Recovery Motion by Use of Rotary Balance Aerodynamic Data, NACA TN 3188
Scher, Stanley H. 1955. Pilot's Loss of Orientation in Inverted Spins, NACA TN 3531
Skow, Andrew M. and G. E. Erickson 1982. Modern Fighter Aircraft Design for High Angle of Attack Maneuvering, in High Angle of Attack Aerodynamics, in AGARD LS-121
Soulé, Hartley A. and N. A. Scudder 1931. A Method of Flight Measurement of Spins. NACA Rept. 377
Stephens, A. V. 1931. Free-Flight Spinning Investigations with Several Models, British R & M 1404
Stephens, A. V. 1966. Some British Contributions to Aerodynamics, Jour. of the Royal Aeronautical Soc., Vol. 70, No. 661, pp. 71–78
Stough, H. Paul III, James M. Patton, Jr., and Steven M. Sliwa 1987. Flight Investigation of Tail Configuration on Stall, Spin, and Recovery Characteristics of a Low-Wing General Aviation Research Airplane, NASA TP-2644
Tobak, Murray and L. B. Schiff 1976. On the Formulation of the Aerodynamic Characteristics in Aircraft Dynamics, NASA TR R-456
Tobak, Murray, G. T. Chapman, and L. B. Schiff 1984. Mathematical Modeling of the Aerodynamic Characteristics in Flight Mechanics, NASA TM-85880
Tristrant, D. and O. Renier 1985. AGARD CP 386, Paper No. 22
Weissman, R. 1974. Status of Design Criteria for Predicting Departure Characteristics, AIAA Paper 74-791
Westbrook, Charles B. and H. K. Doetsch, (eds.) 1957. Trans. of the Wright Air Development Center Airplane Spin Symposium, 57 WCLC-1688 and -1744
Yip, Long P., Ross, Holly M., and Robelen, David R. 1992. Model Flight Tests of a Spin-Resistant Trainer Configuration, Jour. of Aircraft, Vol. 29, No. 5, pp. 799–805
Zimmerman, Charles H. 1936. Preliminary Tests in the NACA Free-Spinning Wind Tunnel, NACA Rept. 557
Chapter 10. Tactical Airplane ManeuverabilityAnon. 1980. Military Specification, Flying Qualities of Piloted Airplanes, MIL-F-8785C
Anon. 1987. Flying Qualities of Piloted Vehicles, MIL-STD-1797, U.S. Air Force
Arena, A. S. Jr., , R. C. Nelson, and Schiff, L. B. 1995. Directional Control at High Angles of Attack Using Blowing Through a Chined Forebody, Jour. of Aircraft, Vol. 32, No. 3, pp. 596–602
Barham, Robert W. 1994. Thrust Vector Aided Maneuvering of the YF-22 Advanced Tactical Fighter Prototype, in AGARD CP 548
Bihrle, William, Jr. 1966. A Handling Qualities Theory for Precise Flight-Path Control, AFFDL-TR-65-198
Chambers, Joseph R. 2000. Partners in Freedom, Monographs in Aerospace History No. 19, NASA SP-2000-4519, p. 41
Blight, James D., R. Lane Dailey, and Dagfinn Gangsass 1996. Practical Control Law Design Using Multivariable Techniques, in Advances in Aircraft Flight Control, ed. By M. B. Tischler, London: Taylor and Francis, pp. 231–267
Ericsson, Lars E. and Byers, Martin E. 1997. Conceptual Fluid/Motion Coupling in the Herbst Supermaneuver, Jour. of Aircraft, Vol. 34, No. 3, pp. 271–277
Field, Edmund J. and Ken F. Rossitto 1999. Approach and Landing Longitudinal Flying Qualities for Large Transports Based on in-Flight Results, AIAA Paper AIAA-99-4095
Gautrey, J. E. and Cook, M. V. 1998. A Generic Control Anticipation Parameter for Aircraft Handling Qualities Evaluation, The Aeronautical Jour., Vol. 102, No. 1013, pp. 151–159
Gibson, John C. 1995. The Definition, Understanding and Design of Aircraft Handling Qualities, TU Delft Report LR-756
Gibson, John C. 2000. Unpublished comments in letter, dated 10 December
Hodgkinson, J., , W. J. LaManna, and Hyde, J. L. 1976. Handling Qualities of Aircraft with Stability and Control Augmentation Systems – A Fundamental Approach, The Aeronautical Jour., Vol. 80, No. 782, pp. 75–81
Hoh, Roger H. and Ashkenas, Irving L. 1977. Handling Quality Criterion for Heading Control, Jour. of Aircraft, Vol. 14, No. 2, pp. 142–150
Hoh, Roger H. and David G Mitchell (1996). Handling-Qualities Specification – A Functional Requirement for the Flight Control System, in Advances in Aircraft Flight Control, ed. M. B. Tischler, London: Taylor and Francis, pp. 3–33
Mangold, Peter 1991. Transformation of Flightmechanical Design Requirements for Modern Fighters into Aerodynamic Characteristics, in AGARD CP-497
Mitchell, David G. and Hoh, Roger H. 1982. Low-Order Approaches to High-Order Systems: Problems and Promises, Jour. of Guidance, Vol. 5, No. 5, pp. 482–488
Myers, Thomas T., D. T. McRuer, and D. E. Johnston 1987. Flying Qualities Analysis for Nonlinear Large Amplitude Maneuvers, AIAA Paper 87-2904
Nguyen, Luat T. and John V. Foster 1990. Development of a Preliminary High Angle of Attack Nose-Down Pitch Control Requirement for High-Performance Aircraft, NASA TM 101684
Pedreiro, Nelson, Rock, Stephen M., Celik, Zeki Z., and Leonard, Roberts 1998. Roll-Yaw Control at High Angle of Attack by Forebody Tangential Blowing, Jour. of Aircraft, Vol. 35, No. 1, pp. 69–77
Ward, Greta N. and Ly, Uy-Loi 1996. Stability Augmentation Design of a Large Flexible Transport Using Nonlinear Parameter Optimization, Jour. of Guidance, Control, and Dynamics, Vol. 19, No. 2, pp. 469–474
Zagainov, G. 1993. High Maneuverability, Theory and Practice, AIAA Paper 93-4737 (1993 Wright Brothers Lecture)
Chapter 11. High Mach Number DifficultiesAnderson, Seth B. and Richard S. Bray 1955. A Flight Evaluation of the Longitudinal Stability Characteristics Associated With the Pitch-Up of a Swept-Wing Airplane in Maneuvering Flight at Transonic Speeds, NACA Rept. 1237
Bilstein, Roger E. 1989, Orders of Magnitude, NASA SP-4406
Chilstrom, Ken, and Penn Leary 1993. Test Flying at Old Wright Field, Omaha: Westchester House Publ
Cook, William H. 1991. The Road to the 707, Bellevue, WA: TYC Publ. Co
Ericson, Albert L. 1942. Investigation of Diving Moments of a Pursuit Airplane in the Ames 16-Foot High Speed Wind Tunnel, NACA WR A-65
Erickson, Albert L. 1943. Wind Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes, NACA WR A-66
Furlong, Chester G. and James G. McHugh 1957. Summary and Analysis of the Low-Speed Longitudinal Characteristics of Swept Wings at High Reynolds Number, NACA Rept. 1339
Gilyard, Glenn B. and John W. Smith 1978. Flight Experience with Altitude Hold and Mach Hold Autopilots on the YF-12 at Mach 3, in NASA CP 2054, Vol. I
Hallion, Richard P. 1981. Test Pilots: The Frontiersmen of Flight, New York: Doubleday
Hallion, Richard P. 1984. On the Frontier: Flight Research at Dryden, 1946–1981, NASA SP-4303
Hood, Manley J., and Julian H. Allen 1943. The Problem of Longitudinal Stability and Control at High Speeds, NACA Rept. 767
Jones, Robert T. 1946. Properties of Low-Aspect-Ratio Pointed Wings at Speeds Below and Above the Speed of Sound, NACA Rept. 835
Loftin, Laurence K., Jr. 1985. Quest for Performance, NASA SP-468
McRuer, Duane T., et al. 1992. Assessment of Flying-Quality Criteria for Air-Breathing Aerospacecraft, NASA CR 4442
Myers, Thomas T., David H. Klyde, Duane T. McRuer, and Greg Larson 1993. Hypersonic Flying Qualities, Wright Laboratory Rept. WL-TR-93-3050
Perkins, Courtland D. 1970. Development of Airplane Stability and Control Technology, Jour. of Aircraft, Vol. 7, No. 4, pp. 290–301
Phillips, Edward H. 1994 (Feb. 21). NTSB: Pilots Need Training for High Altitude Stalls, AWST
Sachs, Gottfried 1990. Effects of Thrust/Speed Dependence on Long-Period Dynamics in Supersonic Flight, Jour. of Guidance, Control, and Dynamics, Vol. 13, No. 6, pp. 1163–1186
Schuebel, F. N. 1942. The Effect of Density Gradient on the Longitudinal Motion of an Aircraft, Luftfahrtforschung, Vol. 19, No. 4, R.T.P Translation 1739
Shevell, Richard S. 1992. Aerodynamic Bugs: Can CFD Spray Them Away?, Aerodynamic Analysis and Design, AIAA Professional Studies Series, Palo Alto, CA: AIAA
Shortal, Joseph A. and Bernard Maggin 1946. Effect of Sweepback and Aspect Ratio on Longitudinal Stability Characteristics of Wings at Low Speeds, NACA TN 1093
Stengel, Robert F. 1970. Altitude Stability in Supersonic Cruising Flight, Jour. of Aircraft, Vol. 7, No. 5, pp. 464–473
Sternfield, Leonard 1947. Some Considerations of the Lateral Stability of High-Speed Aircraft, NACA TN 1282
Chapter 12. Naval Aircraft ProblemsAshkenas, Irving L. and Tulvio S. Durand 1963. Simulation and Analytical Studies of Fundamental Longitudinal Control Problems in Carrier Approach, AIAA Simulation for Aerospace Conf., Columbus, OH
Bezanson, A, F. 1961. Effects of Pilot Technique on Minimum Approach Speed, NATC Rept. PTR AD-3089
Craig, Samuel, Robert Ringland, and Irving L. Ashkenas 1971. An Analysis of Navy Approach Power Compensation Problems and Requirements, STI Rept. 197-1
Drinkwater, Fred J. III and George E. Cooper 1958. A Flight Evaluation of the Factors Which Influence the Selection of Landing Approach Speeds, NASA Memo 10-6-58A
Heffley, Robert K. 1990. Outer-Loop Control Factors for Carrier Aircraft, Robert Heffley Engineering Rept. RHE-NAV-90-TR-1 (Limited Distrib.)
Neumark, S. 1953. Problems of Longitudinal Stability Below Minimum Drag Speed, and Theory of Stability Under Constraint, RAE Rept. Aero. 2504
North, David M. 1993 (Aug. 30) Long Development Phase Nearly Over for Goshawk, AWST
Shields, E. R. and D. J. Phelan 1953. The Minimum Landing Approach Speed of High Performance Aircraft, McDonnell Rept. 3232
White, Maurice D., Bernard A. Schlaff, and Fred J. Drinkwater III 1957. A Comparison of Flight-Measured Carrier-Approach Speeds with Values Predicted by Several Different Criteria for 41 Fighter-Type Airplane Configurations, NACA RM A57L11
Wilson, George C. 1992. Flying the Edge, Annapolis: Naval Institute Press
Chapter 13. Ultra Light and Human Powered AircraftAnderson, Seth B. and Robert A. Ormiston 1994. A Look at Handling Qualities of High Performance Hang Gliders, AIAA Paper 94-3492 CP
Brooks, W. G. 1998. Flight Testing of Flexwings, Aerogram, Cranfield College of Aeronautics, Vol. 9, No. 2, pp. 20–28
Cook, Michael V. and Elizabeth A. Kilkenny 1987. An Experimental Investigation into Methods for Quantifying Hang Glider Airworthiness Parameters, Cranfield Institute of Technology College of Aeronautics Report 8705
Gracey, William 1941. The Additional-Mass Effects of Plates as Determined by Experiments, NACA Rept. 707
Grosser, Morton 1981. Gossamer Odyssey, Boston: Houghton Mifflin Co
Jex, Henry R. 1979. Gossamer Condor Dynamic Stability and Control Analysis, Systems Technology, Inc., Paper 240A
Jex, Henry R. and David G. Mitchell 1982. Stability and Control of the Gossamer Condor Human-Powered Aircraft by Analysis and Flight Test, NASA CR 3627
Mitchell, David G. and Henry R. Jex 1983. Flight Testing the Gossamer Albatross Human-Powered Aircraft, AIAA Paper 83-2699
Roderick, W. E. B. 1986. Wind Tunnel Evaluation of Chinook WT-11 Ultra Light, NAE Aeronautical Note NAE-AN-35, Ottawa
Rogallo, F. M., John G. Lowry, D. R. Croom, and R. T. Taylor 1960. Preliminary Investigation of a Paraglider, NASA TN D-443
Chapter 14. Fuel Slosh, Deep Stall, and MoreAbzug, M. J. 1959. Effects of Fuel Slosh on Stability and Control, Douglas Rept. ES 29551
Abzug, M. J. 1999. Directional Stability and Control During Landing Rollout, Jour. of Aircraft, Vol. 36, No. 3, pp. 584–590
Anderson, Seth B., Einar K. Enevoldson, and Luat T. Nguyen 1983. Pilot Human Factors in Stall/Spin Accidents of Supersonic Fighter Aircraft, in AGARD CP 347
Anon. 1986. Beech Airframe Failure Report (results of flight tests by Prof. Ronald O. Stearman), The 1986 Pilot's Yearbook, pp. 1–7
Archer, Donald D. and Charles L. Gandy, Jr. 1957. T-37A Phase IV Performance and Stability and Control, ATTTC-TR-56-37
Bollay, William 1937. A Theory for Rectangular Wings of Small Aspect Ratio, Jour. of the Aeronautical Sciences, Vol. 4, No. 7, pp. 294–296
Chambers, Joseph R. 2000. Partners in Freedom, Monographs in Aerospace History No. 19, NASA SP-2000-4519, pp. 55, 56, 153
Covert, Eugene E. 1993. Aerodynamic Hysteresis of Two-Dimensional Airfoils and Wings at Low Speed; An Empiricist's View, Advances in Aerospace Sciences, eds. P. Hajela and S. C. McIntosh, Stanford, CA: Stanford U., pp. 81–92
Crawford, Charles C. and Jones P. Seigler 1958. KC-135A Stability and Control Test, AFFTC-TR-58-13
Harper, John A. 1950. DC-3 Handling Qualities Tests, NACA, Paper presented to the Society of Experimental Test Pilots
Fischenberg, D. and R. V. Jategaonkar 1999. Identification of Aircraft Stall from Flight Test Data, RTO MP-11, pp. 17-1–17-8
Hamel, Peter G. and Jategaonkar, Ravindra V. 1996. Evolution of Flight Vehicle System Identification, Jour. of Aircraft, Vol. 33, No. 3, pp. 9–28 (with 183 references)
Hamel, Peter G. and R. V. Jategaonkar 1999. The Role of System Identification for Flight Vehicle Applications – Revisited, RTO MP-11, pp. 2-1–2-12
Heffley, Robert K. and Wayne F. Jewell 1972. Aircraft Handling Qualities Data, NASA CR 2144
Iliff, Kenneth W. and Richard E. Maine 1986. A Bibliography for Aircraft Parameter Estimation, NASA TM 86804
Iliff, Kenneth W. 1989. Parameter Estimation for Flight Vehicles, Jour. of Guidance, Vol. 12, No. 5, pp. 609–622
Katzoff, S. and Harold H. Sweberg 1942. Ground Effect on Downwash and Wake Location, NACA Rept. 738
Koehler, W. and K. Wilhelm 1977. Auslegung von Eingangssignalen für die Kennwertermittlung, DFVLR-IB 154-77/40, December
Luskin, Harold and Lapin, Ellis 1952. An Analytical Approach to the Fuel Sloshing and Buffeting Problems of Aircraft, Jour. of the Aeronautical Sciences, Vol. 19, No. 4, pp. 217–228
Purser, Paul E. and John P. Campbell 1945. Experimental Verification of a Simplified Vee-Tail Theory and Analysis of Available Data on Complete Models with Vee Tails, NACA Rept. 823
Reed, R. Dale 1997. Wingless Flight: The Lifting Body Story, NASA SP 4220, NASA Historical Series
Schairer, George S. 1941. Directional Stability and Vertical Surface Stalling, Jour. of the Aeronautical Sciences, Vol. 8, No. 7, pp. 270–275
Schy, Albert A. 1952. A Theoretical Analysis of the Effects of Fuel Motion on Airplane Dynamics, NACA Rept. 1080
Soderman, Paul T. and Thomas N. Aiken 1971. Full-Scale Wind-Tunnel Tests of a Small Unpowered Jet Aircraft with a T-Tail, NASA TN D-6573
Taylor, Robert T. and Edward J. Ray 1985. Deep-Stall Aerodynamic Characteristics of T-Tail Aircraft, in Conference on Aircraft Operating Problems, NASA SP-63
Weick, Fred C. 1936. Everyman's Airplane – A Move Toward Simpler Flying, S.A.E. Jour. (Transactions), Vol. 38, No. 5, pp. 176–189
Weiss, Suzanne, Friehmelt, Holger, Plaetschke, Ermin, and Rohlf, Detlef 1996. X-31 System Identification Using Single-Surface Excitation at High Angles of Attack, Jour. of Aircraft, Vol. 33, No. 3, pp. 485–490
Wetmore, J. W. and L. I. Turner, Jr. 1940. Determination of Ground Effect from Tests of a Glider in Towed Flight, NACA Rept. 695
Chapter 15. Safe Personal Airplanes,Anon. 1994. Used Aircraft Guide, Piper PA-31T Series Cheyennes, The Aviation Consumer, Vol. 24, No. 9, pp. 4–11
Anon. 1999. Aeronautical Information Manual (AIM), ASA-99-FAR-AM-BK, Aviation Supplies and Academics, Newcastle, WA
Barber, M. R., C. K. Jones, T. R. Sisk, and F. W. Haise 1966, An Evaluation of the Handling Qualities of Seven General-Aviation Aircraft, NASA TN D-3726
Bar-Gill, Aharon and Stengel, Robert F. 1986. Longitudinal Flying Qualities Criteria for Single-Pilot Instrument Flight Operation, Jour. of Aircraft, Vol. 23, No. 2, pp. 111–117
Campbell, John P., Paul A. Hunter, Donald E. Hewes, and James B. Whitten 1952. Flight Investigation of Control Centering Springs on the Apparent Spiral Stability of a Personal-Owner Airplane, NACA Rept. 1092
Ferree, William M. 1994. Lightening Up on Design, Technology Review, MIT, Jan., p. 6
Goode, M. W. et al. 1976. Landing Practices of General Aviation Pilots in Single-Engine Light Airplanes, NASA TN D-8283
Greer, H. Douglas et al. 1973. Wind Tunnel Investigation of Static Longitudinal and Lateral Characteristics of a Full-Scale Mockup of a Light Single-Engine High-Wing Airplane, NASA TN D-7149
Loschke, Paul C. et al. 1974. Flight Evaluation of Advanced Control Systems and Displays on a General Aviation Airplane, NASA TN D-7703
Pendray, G. Edward 1964. The Guggenheim Medalists 1929–1963, New York: The Guggenheim Board of Award of the United Engr. Trustees, Inc
Phillips, W. H., Helmut A. Kuehnel, and James B. Whitten 1957. Flight Investigation of the Effectiveness of an Automatic Aileron Trim Control Device for Personal Airplanes, NACA Rept. 1304
Phillips, W. H. 1998. Journey in Aeronautical Research, Monographs in Aerospace History, Number 12, Washington, DC: NASA
Picon, Gary 1994. Autopilot Buyer's Guide, The Aviation Consumer, July 1
Regis, Edward 1995. Spratt, Schmittle, and Freewing, Air & Space, Vol. 9, No. 5, pp. 58–65
Upson, Ralph H. 1942. New Developments in Simplified Control, Jour. of the Aeronautical Sciences, Vol. 9, No. 14, pp. 515–520, 548
Chapter 16. Stability and Control Issues With Variable SweepKroo, Ilan 1992. The Aerodynamic Design of Oblique Wing Aircraft, AIAA Professional Studies Series, Palo Alto, CA: AIAA
Loftin, Laurence H., Jr. 1985. Quest for Performance, NASA SP 468
Nelms, W. 1976. Applications of Oblique Wing Technology, AIAA Paper 76-943
Nguyen, Luat T. et al. 1980. Application of High Angle of Attack Control System Concepts to a Variable-Sweep Fighter Airplane, AIAA Paper 80-1582-CP
Polhamus, Edward C. and Thomas A. Toll 1981. Research Related to Variable Sweep Aircraft Development, NASA TM 83121
Chapter 17. Modern Canard ConfigurationsAgnew, J. W., G. W. Lyerla, and Sue B. Grafton 1980. Linear and Nonlinear Aerodynamics of 3-Surface Aircraft Concepts, AIAA Paper 80-1581-CP
Chambers, Joseph R. and Long P. Yip 1984. Aerodynamic Characteristics of Two General Aviation Canard Configurations at High Angles of Attack, AIAA Paper 84-2198
Jones, B. Melvill 1934. Dynamics of the Airplane, in Aerodynamic Theory, Vol. V, ed. W. F. Durand, Berlin: Springer, pp. 208–214
Lorincz, D. J. 1980. Flow Visualization of the HiMat RPV, NASA CR-163094
McCormick, Barnes W. 1979. Aerodynamics, Aeronautics, and Flight Mechanics, New York: Wiley, pp. 613–617
Yeager, Jeana, Dick Rutan, and Phil Patton 1987. Voyager, New York: Knopf
Yip, Long P. 1985. Wind-Tunnel Investigation of a Full-Scale Canard-Configured General Aviation Airplane, NASA TP-2382
Chapter 18. Evolution of the Equations of MotionAbzug, M. J. 1998. Computational Flight Dynamics, AIAA Education Series, Reston, VA: AIAA, pp. 105, 106
Abzug, M. J. 1980. Hinged Vehicle Equations of Motion, AIAA Paper 80-0364
Abzug, M. J. and W. P. Rodden 1993. The Centroidal Siren and Computational Flight Mechanics, in Advances in Aerospace Sciences, Stanford, CA: Stanford Univ
Anon. 1996. AIAA Guide to Reference and Standard Atmospheric Models, G-003A-1996, VA: Reston, AIAA
Ashkenas, Irving L. and Duane T. McRuer 1958. Approximate Airframe Transfer Functions and Application to Single-Sensor Control Systems, WADC Technical Report 58-82, Wright-Patterson Air Force Base, Ohio
Bairstow, Leonard, J. L. Nayler, and R. Jones 1914. Investigation of the Stability of an Aeroplane when in Circling Flight, British R & M 154
Bairstow, Leonard 1920. Applied Aerodynamics, London: Longmans, Green and Co
Beam, Benjamin H. 1956. A Wind-Tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives at Subsonic and Supersonic Speeds, NASA Rept. 1258
Bernstein, L. 1998. On the Equations of Motion for an Aircraft with an Internal Moving Load Which is then Dropped, The Aeronautical Jour., Vol. 102, No. 1011, pp. 9–24
Bray, Richard S. 1984. A Method for Three-Dimensional Modeling of Wind-Shear Environments for Flight Simulator Applications, NASA TM 85969
Bryan, G. H. and W. E. Williams 1903. The Longitudinal Stability of Aerial Gliders, Proc. of the Royal Soc., Ser. A, 73, No. 489
Bryant, L. W., I. M. W. Jones, and G. L. Pawsey 1932. The Lateral Stability of an Aeroplane Beyond the Stall, British R & M 1519
Bryant, L. W. and S. B. Gates 1937. Nomenclature for Stability Coefficients, British R & M 1801
Chen, Robert T. N. 1983. Efficient Algorithms for Computing Trim and Small-Disturbance Equations of Motion of Aircraft in Coordinated and Uncoordinated, Steady, Steep Turns, NASA TM 84324
Cook, M. V., Lipscombe, J. M., and Goineau, F. (2000). Analysis of the Stability Modes of the Non-Rigid Airship, The Aeronautical Journal, Vol. Vol. 104, No. 1036, pp. 279–290
Frazer, R. A., W. J. Duncan, and A. R. Collar 1950. Elementary Matrices, London: Cambridge U. Press
Gates, Sidney B. 1927. A Survey of Longitudinal Stability Beyond the Stall, with an Abstract for Designer's Use, British R & M 1118
Glauert, H. 1927. A Nondimensional Form of the Stability Equations of an Aeroplane, British R & M 1093
Heffley, Robert K. and Wayne F. Jewell 1972. Aircraft Handling Qualities Data, NASA CR 2144
Hopkin, H. R. 1966. A Scheme of Notation and Nomenclature for Aircraft Dynamics and Associated Aerodynamics, RAE Tech. Rept. 66200
ICAO, 1955. Standard Atmosphere – Tables and Data for Altitudes to 65,800 Feet, NACA Rept. 1235
ICAO, 1962. U.S. Standard Atmosphere, 1962, NASA, USAF, U.S. Weather Bureau, Washington, DC
Johnson, Walter A., Teper, Gary L., and Rediess, Herman A. 1974. Study of Control System Effectiveness in Alleviating Vortex Wake Upsets, Jour. of Aircraft, Vol. 11, No. 3, pp. 148–154
Jones, B. M. and A. Trevelyan 1925. Step-by-Step Calculations Upon the Asymmetric Movements of Stalled Airplanes, British R & M 999
Jones, B. M. 1934. Dynamics of the Aeroplane, Divsion N of Aerodynamic Theory, Vol. V, ed. by W. F. Durand, California, Durand Reprinting Committee
Jones, Robert T. 1936. A Simplified Application of the Method of Operators to the Calculation of the Disturbed Motion of an Airplane, NACA TR 560
Kamesh, S. and Pradeep, S. 1999. Phugoid Approximation Revisited, Jour. of Aircraft, Vol. 36, No. 2, pp. 465–467
Lehman, John M., Robert K. Heffley, and Warren F. Clement 1977. Simulation and Analysis of Wind Shear Hazard, FAA-RD-78-7
McMinn, John D, and John D. Shaughnessy 1991. Atmospheric Disturbance Model for NASP Applications, in NACA TM 4331
McRuer, Duane, Irving L. Ashkenas, and Dunstan Graham 1973. Aircraft Dynamics and Automatic Control, Princeton, NJ: Princeton U. Press, pp. 296–316, 353–380
Melsa, James L. and Stephen K. Jones 1973. Computer Programs for Computational Assistance in the Study of Linear Control Theory, New York: McGraw-Hill
Milne-Thomson, M. 1958. Theoretical Aerodynamics, London: Macmillan
Mokrzycki, G. A. 1950. Application of the Laplace Transformation to the Solution of the Lateral and Longitudinal Stability Equations, NACA TN 2002
Mueller, Robert K. 1937. The Graphical Solution of Stability Problems, Jour. of the Aeronautical Sciences, Vol. 4, No. 8, pp. 324–331
Mulkens, Marc J. M. and Ormerod, Albert O. 1993. Measurements of Aerodynamic Rotary Stability Derivatives Using a Whirling Arm Facility, Jour. of Aircraft, Vol. 30, No. 2, p. 178
Myers, Thomas T., David H. Klyde, Duane T. McRuer, and Greg Larson 1993. Hypersonic Flying Qualities, WL-TR-93-3050
Neumark, S. 1957. Problems of Longitudinal Stability Below Minimum Drag Speed and Theory of Stability Under Constraint, British R & M 2983
Newell, F. D. 1965. Ground Simulator Evaluations of Coupled Roll-Spiral Mode Effects on Aircraft Handling Qualities, AFFDL-TR-65-39
Phillips, W. F. 2000. Improved Closed-Form Approximation for Dutch Roll, Jour. of Aircraft, Vol. 37, No. 3, pp. 484–490
Phillips, W. F., , C. E. Hailey, and Gebert, G. A. 2001. Review of Attitude Representations Used for Airplane Kinematics, Jour. of Aircraft, Vol. 38, No. 4, pp. 718–737, (168 references)
Pinsker, W. J. G. 1967. Directional Stability in Flight with Bank Angle Constraint as a Condition Defining a Minimum Acceptable Value for nv, RAE Tech. Rept. 67-127
Powers, Bruce G. and Lawrence J. Schilling 1980, 1985. Subroutine DERIVC [of the SIM2 program], NASA Dryden Research Center
Regan, Frank J. and Satya M. Anandakrishnan 1993. Dynamics of Atmospheric Re-Entry, AIAA Education Series, Washington, DC: AIAA, p. 395
Ribner, Herbert S. 1956. Spectral Theory of Buffeting and Gust Response: Unification and Extension, Jour. of the Aeronautical Sciences, Vol. 23, No. 12, pp. 1075–1077, 1118
Robinson, A. C. 1957. On the Use of Quaternions in Simulation of Rigid Body Motion, Wright Air Development Center Rept. TR-58-17
Schilling, Lawrence J., Marlin D. Pickett, and David M. Aubertin 1993. The NASP Integrated Atmospheric Model, 1993 National Aero-Space Plane Technology Review, Monterey, CA., NASA Publication GWP-ZAA
Spilman, Darin R. and Stengel, Robert F. 1995. Jet Transport Response to a Horizontal Wind Vortex, Jour. of Aircraft, Vol. 32, No. 3, pp. 480–485
Sternfield, Leonard 1947. Some Considerations of the Lateral Stability of High-Speed Aircraft, NACA TN 1282
Stevens, Brian L. and Frank L. Lewis 1992. Aircraft Control and Simulation, New York: Wiley, pp. 132–139
Strumpf, Albert 1979. Stability and Control, Hydroballistics Design Handbook, Vol. 1, SEAHAC TR 79-1
Teper, Gary L. 1969. Aircraft Stability and Control Data, NASA CR 96008
Thelander, J. A. 1965. Aircraft Motion Analysis, FDL-TR-64-70
Workman, F. 1924. Analysis of the Motion of an SE 5 Aeroplane by Step-by-Step Integration, Unpublished Report of the British A.R.C. (T 1918)
Zimmerman, Charles H. 1935. An Analysis of Longitudinal Stability in Power-Off Flight With Charts for Use in Design, NACA Rept. 521
Zimmerman, Charles H. 1937. An Analysis of Lateral Stability in Power-Off Flight With Charts for Use in Design, NACA Rept. 589
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Doyle, John C. and Stein, Gunter 1981. Multivariable Feedback Design: Concepts for a Classical/Modern Synthesis, IEEE Transactions on Automatic Control, Vol. AC-26, No. 1, pp. 4–16
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Steer, A. J. 2000. Low Speed Control of a Second Generation Supersonic Transport Aircraft Using Integrated Thrust Vectoring, The Aeronautical Journal, Vol. 104, No. 1035, pp. 237–245
Stengel, Robert F. and Berry, Paul W. 1977. Stability and Control of Maneuvering High-Performance Aircraft, Jour. of Aircraft, Vol. 14, No. 8, pp. 787–794
Stengel, Robert F. 1986. Stochastic Optimal Control, New York: Wiley
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Whitbeck, R. F., and , L. G. Hofmann 1978. Digital Law Synthesis in the w' Domain, Jour. of Guidance and Control, Vol. 1, No. 5, pp. 319–326
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White, Roland J. 1950. Investigation of Lateral Dynamic Stability in the XB-47 Airplane, Jour. of the Aeronautical Sciences, Vol. 17, No. 3, pp. 133–148
Chapter 21. Flying Qualities Research Moves with the TimesAnderson, M. R. and Schmidt, D. K. 1987. Closed-Loop Pilot Vehicle Analysis of the Approach and Landing Task, Jour. of Guidance, Control, and Dynamics, Vol. 10, No. 2, pp. 187–194
Ashkenas, Irving L., Jex, Henry R., and Teper, Gary L. 1984. Analysis of Shuttle Orbiter Approach and Landing, Jour. of Guidance, Control, and Dynamics, Vol. 7, No. 1, pp. 106–112
Ashkenas, Irving L. 1988. Pilot Modeling Applications, in Advances in Flying Qualities, AGARD Lecture Series LS-157
Aviation Safety and Pilot Control 1997. Report of the Committee on the Effects of Aircraft-Pilot Coupling on Flight Safety, Washington, DC: National Academy Press
Dornheim, Michael A. 1993 (May 4). Report Pinpoints Factors Leading to YF-22 Crash, AWST, pp. 52–54
Grey, Jerry 2000. Monitoring Aircraft in Real Time, Aerospace America, Vol. 38, No. 11, pp. 36–40
Gibson, John 1999. Development of a Methodology for Excellence in Handling Qualities Design for Fly by Wire Aircraft, Series 03 Control and Simulation 06, Delft University Press
Gibson, John C. 2000. Unpublished comments in letter, dated 10 December
Hess, Ronald A. 1976. A Method for Generating Numerical Pilot Opinion Ratings Using the Optimal Pilot Model, NASA TM X-73101
Hess, Ronald A. 1990. Methodology for the Analytical Assessment of Aircraft Handling Qualities, Control and Dynamic Systems, Vol. 33, No. 3, pp. 129–149
Hoh, Roger H. 1988. Advances in Flying Qualities, Advances in Flying Qualities, AGARD Lecture Series 157
Kleinman, D. L., Baron, S., and Levinson, W. H. 1970. An Optimal Control Model of Human Response, Automatica, Vol. 6, No. 3, pp. 357–383
McRuer, Duane T. 1973. Human Operator System and Subsystem Dynamic Characteristics, Regulation and Control in Physiological Systems, Pittsburgh, PA: Instr. Soc. of Amer., pp. 230–235
McRuer, Duane T. 1973. Development of Pilot-in-the-Loop Analysis, Jour. of Aircraft, Vol. 10, No. 9, pp. 515–524
McRuer, Duane T. and E. S. Krendel 1974. Mathematical Models of Human Pilot Behavior, AGARDograph. No. 188
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McRuer, Duane T. and Schmidt, David K. 1990. Pilot-Vehicle Analysis of Multi-Axis Task, Jour. of Guidance, Control, and Dynamics, Vol. 13, No. 2, pp. 348–355
McRuer, Duane T. 1990. Pilot-Vehicle Analysis of Multiaxis Tasks, Jour. of Guidance, Vol. 13, No. 2, pp. 348–355
McRuer, Duane T. et al. 1990. Pilot Modeling for Flying Qualities Applications, Minimum Flying Qualities, Vol II, WRDC-TR-89-3125
McRuer, Duane T. 1992. Human Dynamics and Pilot-Induced Oscillations, 22nd Minta Martin Lecture, MIT
McRuer, Duane T. 1994. Pilot-Induced Oscillations and Human Dynamic Behavior, NASA CR 4683
MrRuer, Duane T. (chair) 1997. Report of the Committee on the Effects of Aircraft-Pilot Coupling on Flight Safety, Washington, DC: National Academy Press
Moorhouse, David J. and Robert J. Woodcock 1982. Present Status of Flying Qualities Criteria for Conventional Aircraft, Criteria for Handling Qualities of Military Aircraft, AGARD CP 333
Neil, T. Peter and Rogers E. Smith 1970. An In-Flight Investigation to Develop Control System Design Criteria for Fighter Airplanes, AFFDL-TR-70-74, Vol. I
Smith, Ralph H. and Norman D. Geddes 1979. Handling Quality Requirements for Advanced Aircraft Design: Longitudinal Mode, AFFDL-TR-78-154
Stengel, Robert F and Broussard, John R. 1978. Prediction of Pilot-Aircraft Stability Boundaries and Performance Contours, IEEE Transactions on Systems, Man, and Cybernetics, Vol. SMC-8, No. 5, pp. 349–356
Thompson, Peter M. and Duane T. McRuer 1988. Comparison of the Human Optimal Control and Crossover Models, AIAA Paper 88-4183, AIAA Guidance, Navigation and Control Conf., Minneapolis
Chapter 22. Challenge of Stealth AerodynamicsFarley, Harold C., Jr. and Richard Abrams 1990. F-117A Flight Test Program, Thirty-Fourth Symposium Proceedings, Beverly Hills, CA: Soc. of Experimental Test Pilots, pp. 141–167
Fulghum, David A. 1994 (Mar. 14). F-22 Signature Problem Inflicts Weight Penalty, AWST, pp. 30, 31
Oliveri, Frank 1994 (Mar.). Fundamental Features for Future Fighters, Air Force Magazine, pp. 36–40
Pace, Steve 1992. The F-117A – The Stealth Fighter, Blue Ridge Summit, PA: TAB/Aero Books
Chapter 23. Very Large AircraftCleveland, F. A. 1970. Size Effects in Conventional Aircraft Design, Jour. of Aircraft, Vol. 17, No. 6, pp. 483–512
Condit, P. M., L. G. Kimbrel, and R. G. Root 1966. In-Flight and Ground-Based Simulation of Handling Qualities of Very Large Airplanes in Landing Approach, NASA CR 635
Gibson, John 1995. The Definition, Understanding and Design of Aircraft Handling Qualities, TU Delft Report LR-756
Grantham, William D. 1983. Large Aircraft Handling Qualities, First Annual NASA Aircraft Controls Workshop, Hampton, VA
Grantham, William D., Paul M. Smith, Perry L. Deal, and William R. Neely, Jr. 1984. Simulator Study of Several Large, Dissimilar, Cargo Transport Airplanes During Approach and Landing, NASA TP 2357
Grantham, William D., Paul M. Smith, Lee H. Person, Jr., Robert T. Meyer, and Stephen A Tingas 1987. Piloted Simulator Study of Allowable Time Delays in Large-Airplane Response, NASA TP 2652
Holleman, Euclid C. and Bruce G. Powers 1972. Flight Investigation of the Roll Requirements for Transport Airplanes in the Landing Approach, NASA TN D-7062
Mueller, Lee J. 1970. Pilot and Aircraft Augmentation, Jour. of Aircraft, Vol. 7, No. 6, pp. 553–556
Phillips, William H. 1979. Altitude Response of Several Airplanes During Landing Approach, NASA TM 80186
Pinsker, W. J. G. 1969. The Landing Flare of Large Transport Aircraft, British R & M 3602
Powers, Bruce G. 1986. Space Shuttle Longitudinal Landing Flying Qualities, Jour. of Guidance, Vol. 9, No. 5
Proctor, Paul 1994 (Feb. 21). Super-Jumbos Pose Design Challenges, AWST
Steer, A. J. and Cook, M. V. 1999. Control and Handling Qualities Considerations for an Advanced Supersonic Transport Aircraft, The Aeronautical Jour., Vol. 103, No. 1024, pp. 265–271
Ward, Greta and Uy-Loi, Ly 1996. Stability Augmentation Design of a Large Flexible Transport Using Nonlinear Parameter Optimization, Jour. of Guidance, Control, and Dynamics, Vol. 19, No. 2, pp. 469–474
Woodcock, Robert J. 1988. A Second Look at MIL Prime Flying Qualities Requirements, Advances in Flying Qualities, AGARD Lecture Series LS-157
