Livres : « Lateral Stability Control »

1

Jouma'a, Mohamed. Aerodynmaic interference and lateral stability and control. Manchester : University ofManchester, 1995.

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2

Thomas, Carpenter, et Dryden Flight Research Facility, dir. Thrust vectoring for lateral-directional stability. Edwards, Calif : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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3

Schiess, James R. Lateral stability and control derivatives extracted from space shuttle data. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1988.

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4

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., dir. Relative control effectiveness technique with application to airplane control coordination. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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5

Suit, William T. Lateral and longitudinal stability and control parameters for the space shuttle Discovery as determined from flight test data. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1988.

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6

A, Jeske James, Hardy Gordon H et Ames Research Center, dir. Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA). Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1990.

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7

A, Jeske James, Hardy Gordon H et Ames Research Center, dir. Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA). Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1990.

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8

Stephenson, Jack D. Lateral-directional stability and control characteristics of the quiet short-haul research aircraft (QSRA). Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 1990.

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9

Franklin, James A. V/STOL dynamics, control, and flying qualities. Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, 2000.

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10

Suit, William T. Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1986.

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11

Schiess, James R. Lateral stability and control derivatives extracted from five early flights of the Space Shuttle Columbia. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 1986.

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12

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, 1996.

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13

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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14

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. Washington, D.C : National Aeronautics and Space Administration, 1996.

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15

Charles, Wang Kon-Sheng, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., dir. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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16

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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17

Iliff, Kenneth W. X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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18

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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19

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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20

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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21

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center, 1997.

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22

Iliff, Kenneth W. Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack. [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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23

J, Glaab Louis, et Langley Research Center, dir. Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 2000.

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24

L, Berrier Bobby, et United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., dir. Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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25

Reubush, David E. Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. Hampton, Va : Langley Research Center, 1987.

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26

Charles, Wang Kon-Sheng, et Hugh L. Dryden Flight Research Center., dir. Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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27

Charles, Wang Kon-Sheng, et Hugh L. Dryden Flight Research Center., dir. Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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28

Charles, Wang Kon-Sheng, et Hugh L. Dryden Flight Research Center., dir. Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivates. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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29

Iliff, Kenneth W. Flight-determined, subsonic, lateral-directional stability and control derivatives of the thrust-vectoring F-18 high angle of attack research vehicle (HARV), and comparisons to the basic F-18 and predicted derivatives. Edwards, Calif : National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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30

George C. Marshall Space Flight Center., dir. Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept. MSFC, Ala : National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.

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31

National Aeronautics and Space Administration (NASA) Staff. Lateral-Directional Stability and Control Characteristics of the Quiet Short-Haul Research Aircraft (Qsra). Independently Published, 2018.

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32

Experimental and numerical optimization of a high-lift system to improve low-speed performance, stability, and control of an arrow-wing supersonic transport. Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, 2000.

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33

Experimental Determination of the Effect of Negative Dihedral on Lateral Stability and Control Characteristics at High Lift Coefficients. Creative Media Partners, LLC, 2021.

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34

National Aeronautics and Space Administration (NASA) Staff. Lateral and Longitudinal Stability and Control Parameters for the Space Shuttle Discovery As Determined from Flight Test Data. Independently Published, 2018.

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35

Determination of stability and control derivatives for the NASA F/A-18 HARV from flight data using the maximum likelihood method : Progress report. Morgantown, WV : West Virginia University, 1995.

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36

Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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37

Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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38

National Aeronautics and Space Administration (NASA) Staff. Flight-Determined, Subsonic, Lateral-Directional Stability and Control Derivatives of the Thrust-Vectoring F-18 High Angle of Attack Research Vehicle (Harv), and Comparisons to the Basic F-18 and Pred. Independently Published, 2018.

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39

Koops, Egbert. Price Setting and Other Attempts to Control the Economy. Sous la direction de Paul J. du Plessis, Clifford Ando et Kaius Tuori. Oxford University Press, 2016. http://dx.doi.org/10.1093/oxfordhb/9780198728689.013.45.

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Prices in the Roman economy were generally set by the operation of free market forces. Occasional government interventions in the form of price ceilings occurred in times of crisis, to stabilise volatile or politically important markets, or to signal moral policies. The mechanism of price formation was generally understood, but price shocks were expected to be curbed. In a similar vein, the valuation techniques developed by the Roman jurists were based on “true” prices rather than pure market prices. Even so, party autonomy in price setting was the norm. The grain market was guided to some extent for obvious political reasons, but even here there was room for private initiative. The freedom to contract was stressed as late as Diocletian, but, not much later, rampant inflation forced him to issue his edict on maximum prices, which remains an exceptional regulation in many ways.

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40

Miller, Nicholas R. Social Choice Theory and Legislative Institutions. Oxford University Press, 2016. http://dx.doi.org/10.1093/acrefore/9780190228637.013.1.

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This is an advance summary of a forthcoming article in the Oxford Research Encyclopedia of Politics. Please check back later for the full article.Narrowly understood, social choice theory is a specialized branch of applied logic and mathematics that analyzes abstract objects called preference aggregation functions, social welfare functions, and social choice functions. But more broadly, social choice theory identifies, analyzes, and evaluates rules that may be used to make collective decisions. So understood, social choice is a subfield of the social sciences that examines what may be called “voting rules” of various sorts. While social choice theory typically assumes a finite set of alternatives over which voter preferences are unrestricted, the spatial model of social choice assumes that policy alternatives can be represented by points in a space of one or more dimensions, and that voters have preferences that are plausibly shaped by this spatial structure.Social choice theory has considerable relevance for the study of legislative (as well as electoral) institutions. The concepts and tools of social choice theory make possible formal descriptions of legislative institutions such as bicameralism, parliamentary voting procedures, effects of decision rules (e.g., supramajority vs. simple majority rule and executive veto rules), sincere vs. strategic voting by legislators, agenda control, and other parliamentary maneuvers. Spatial models of social choice further enrich this analysis and raise additional questions regarding policy stability and change. Spatial models are used increasingly to guide empirical research on legislative institutions and processes.

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