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1

Delp, Frank. Aircraft propellers and controls. Casper, WY: IAP, Inc., 1992.

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2

Stevens, Brian L., Frank L. Lewis, and Eric N. Johnson. Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems. Hoboken, NJ, USA: John Wiley & Sons, Inc, 2015. http://dx.doi.org/10.1002/9781119174882.

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3

Jaw, Link C. Aircraft engine controls: Design, system analysis, and health monitoring. Reston, VA: American Institute of Aeronautics and Astronautics, 2009.

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4

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of combat aircraft controls and of ground effects. Neuilly sur Seine, France: AGARD, 1990.

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5

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamics of combat aircraft controls and of ground effects. Neuilly-sur-Seine: AGARD, 1990.

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6

FEDERAL AVIATION ADMINISTRATION. Quality assurance controls for product acceptance software. [Washington, D.C.] (800 Independence Ave., S.W., Washington 20591): U.S. Dept. of Transportation, Federal Aviation Administration, 1993.

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7

Biezad, Daniel J. Controls design with crossfeeds for hovering rotcract using quantitative feedback theory. [Washington, DC: National Aeronautics and Space Administration, 1994.

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8

Biezad, Daniel J. Controls design with crossfeeds for hovering rotorcraft using quantitative feedback theory. [Washington, DC: National Aeronautics and Space Administration, 1994.

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9

United States. President (1989-1993 : Bush). Veto--Senate Joint Resolution 113: Message from the President of the United States returning without my approval Senate Joint Resolution 113, a joint resolution that would prohibit the export of certain technology, defense articles, and defense services in connection with the codevelopment and coproduction of the FS-X aircraft with Japan. Washington: U.S. G.P.O., 1989.

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10

United States. President (1989-1993 : Bush). Veto--Senate Joint Resolution 113: Message from the President of the United States returning without my approval Senate Joint Resolution 113, a joint resolution that would prohibit the export of certain technology, defense articles, and defense services in connection with the codevelopment and coproduction of the FS-X aircraft with Japan. Washington: U.S. G.P.O., 1989.

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11

Bush), United States President (1989-1993 :. Veto--Senate Joint Resolution 113: Message from the President of the United States returning without my approval Senate Joint Resolution 113, a joint resolution that would prohibit the export of certain technology, defense articles, and defense services in connection with the codevelopment and coproduction of the FS-X aircraft with Japan. Washington: U.S. G.P.O., 1989.

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12

United States. President (1989-1993 : Bush). Veto--Senate Joint Resolution 113: Message from the President of the United States returning without my approval Senate Joint Resolution 113, a joint resolution that would prohibit the export of certain technology, defense articles, and defense services in connection with the codevelopment and coproduction of the FS-X aircraft with Japan. Washington: U.S. G.P.O., 1989.

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13

Bauer, Jeffrey E. Flight test of the X-29A at high angle of attack: flight dynamics and controls. Edwards, Calif: Dryden Flight Research Facility, 1995.

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14

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Technical evaluation report on aerodynamics of combat aircraft controls and of ground effects. Neuilly-sur-Seine: AGARD, 1991.

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15

Flandro, G. A. Dynamic interactions between hypersonic vehicle aerodynamics and propulsion system performance: Final report to Aircraft Guidance and Controls Branch, Guidance and Control Division ... [Washington, DC: National Aeronautics and Space Administration, 1992.

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16

Roskam, Jan. Design, analysis and control of large transports so that control of engine thrust can be used as a back-up of the primary flight controls: Final technical report, grant #NAG 2-789. Lawrence, Kan: University of Kansas, Center for Research, Inc., 1995.

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17

United States. Congress. House. Committee on Government Reform. Subcommittee on National Security, Emerging Threats, and International Relations. Nonproliferation: Assessing missile technology export controls : hearing before the Subcommittee on National Security, Emerging Threats and International Relations of the Committee on Government Reform, House of Representatives, One Hundred Eighth Congress, second session, March 9, 2004. Washington, DC: U.S. G.P.O., 2004.

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18

Office, General Accounting. Export controls: Assessment of Commerce Department's report on missile technology controls : report to the Congress. Washington, D.C: The Office, 1988.

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19

Smoothy, Peter. Radio control aircraft. Hemel Hempstead: Argus, 1989.

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20

Durham, Wayne, Kenneth A. Bordignon, and Roger Beck. Aircraft Control Allocation. Chichester, UK: John Wiley & Sons, Ltd, 2016. http://dx.doi.org/10.1002/9781118827789.

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21

Office, General Accounting. Export controls: Sensitive machine tool exports to China. Washington, D.C: The Office, 1996.

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22

L, Lewis Frank, ed. Aircraft control and simulation. New York: Wiley, 1992.

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23

1950-, Stojić R., ed. Modern aircraft flight control. Berlin: Springer-Verlag, 1988.

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24

Vukobratović, Miomir, and Radoslav Stojić, eds. Modern Aircraft Flight Control. Berlin/Heidelberg: Springer-Verlag, 1988. http://dx.doi.org/10.1007/bfb0043099.

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25

L, Lewis Frank, ed. Aircraft control and simulation. 2nd ed. Hoboken, N.J: J. Wiley, 2003.

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26

Benoit, Andre. Aircraft trajectories: Computation - prediction - control. Neuilly sur Seine, France: AGARD, 1990.

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27

Control of spacecraft and aircraft. Princeton, N.J: Princeton University Press, 1994.

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28

Yakovlev, Andrey Vyacheslavovich, Andrey Sergeevich Istomin, Dmitry Alexandrovich Zatuchny, and Yury Grigorievich Shatrakov. Conditional Function Control of Aircraft. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-1059-2.

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29

Office, General Accounting. Export controls: U.S. controls on trade with selected Middle Eastern countries : fact sheet for the Chairman, Subcommittee on Oversight, Committee on Ways and Means, House of Representatives. Washington, D.C: U.S. General Accounting Office, 1991.

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30

Hopper, David John Frederick. Active control of V/Stol aircraft. Salford: University of Salford, 1990.

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31

C, Chenoweth C., ed. Aircraft flight control actuation system design. Warrendale, PA: Society of Automotive Engineers, 1993.

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32

Langton, Roy. Stability and Control of Aircraft Systems. Chichester, England: John Wiley & Sons Ltd, 2006. http://dx.doi.org/10.1002/9780470058480.

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33

Blakelock, John H. Automatic control of aircraft and missiles. 2nd ed. New York: Wiley, 1991.

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34

Burcham, Frank W. Controlling crippled aircraft--with throttles. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1991.

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35

Johnson, Eric N., Frank L. Lewis, and Brian L. Stevens. Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems. Wiley & Sons, Incorporated, John, 2015.

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36

Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems. Wiley & Sons, Limited, John, 2016.

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37

Johnson, Eric N., Frank L. Lewis, and Brian L. Stevens. Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems. Wiley & Sons, Incorporated, John, 2015.

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38

John, Bull, and Ames Research Center, eds. Piloted simulation tests of propulsion control as backup to loss of primary flight controls for a B747-400 jet transport. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1997.

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39

Integrated flight and propulsion controls for advanced aircraft configurations. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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40

An aircraft model for the AIAA controls design challenge. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1991.

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41

D, España Martín, and United States. National Aeronautics and Space Administration., eds. On the use of controls for subsonic transport performance improvement: Overview and future directions. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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42

K, Drummond Colin, and Lewis Research Center, eds. STOVL aircraft simulation for integrated flight and propulsion controls research. [Cleveland, Ohio?]: National Aeronautics and Space Administration, Lewis Research Center, 1990.

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43

United States. National Aeronautics and Space Administration., ed. Overview of NASA research in fiber optics for aircraft controls. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

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44

E, Fortin Paul, and United States. National Aeronautics and Space Administration., eds. An integrated study of structures, aerodynamics, and controls on the forward swept wing X-29A and the oblique wing research aircraft. Lawrence, Kan: University of Kansas, Center for Research, 1987.

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45

United States. National Aeronautics and Space Administration., ed. Alleviation of whirl-flutter on a joined-wing tilt-rotor aircraft configuration using active controls. [Alexandria, Va.]: American Helicopter Society, 1991.

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46

United States. National Aeronautics and Space Administration., ed. Aerodynamic heating rate distributions induced by trailing edge controls on hypersonic aircraft configurations at Mach 8. [Washington, DC?: National Aeronautics and Space Administration, 1985.

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47

United States. National Aeronautics and Space Administration., ed. The coupling of fluids, dynamics, and controls on Advanced Architecture Computers. [Washington, DC: National Aeronautics and Space Administration, 1995.

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48

The coupling of fluids, dynamics, and controls on Advanced Architecture Computers. [Washington, DC: National Aeronautics and Space Administration, 1995.

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49

B, Davidson John, Murphy Patrick C, and Langley Research Center, eds. A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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50

B, Davidson John, Murphy Patrick C, and Langley Research Center, eds. A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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