TERMIUM Plus^®

Fiche 1,  Justifications,  Anglais

Record number: 1, Textual support number: 1 DEF

A circular pattern of air current created by the movement of an airfoil through the air when the airfoil is generating lift.  4, fiche 1, Anglais, - wing%2Dtip%20vortex

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As an airfoil moves through the atmosphere in sustained flight, an area of high pressure is created beneath it and an area of low pressure is created above it. The air flowing from the high-pressure area to the low-pressure area around and about the tips of the airfoil tends to roll up into two rapidly rotating vortices, cylindrical in shape. These vortices are the predominant parts of aircraft wake turbulence and their rotational force is dependent upon the wing loading, gross weight, and speed of the generating aircraft. The vortices from medium to heavy aircraft can be of extremely high velocity and hazardous to smaller aircraft.  4, fiche 1, Anglais, - wing%2Dtip%20vortex

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wing-tip vortex: term and definition standardized by the Glossary for Pilots and Air Traffic Services Personnel Committee.  5, fiche 1, Anglais, - wing%2Dtip%20vortex

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vortex: The plural forms are "vortexes" and "vortices."  6, fiche 1, Anglais, - wing%2Dtip%20vortex

Fiche 1,  Justifications,  Français

Record number: 1, Textual support number: 1 DEF

Courant d'air circulaire créé par le déplacement d'un profil générateur de portance.  5, fiche 1, Français, - tourbillon%20en%20bout%20d%27aile

Record number: 1, Textual support number: 1 OBS

Lorsqu'un tel profil est déplacé de façon continue dans l'atmosphère, une zone de haute pression se crée à l'intrados et une autre de basse pression se crée sur l'extrados. L'air qui circule autour des ailes, de la zone de haute pression vers celle de basse pression, a tendance à former deux tourbillons cylindriques en rotation rapide. Ces tourbillons produisent la majeure partie de la turbulence de sillage d'un aéronef. La force de rotation de ces tourbillons dépend de la charge alaire, de la masse brute et de la vitesse de l'aéronef. Les tourbillons provoqués par les aéronefs moyens et lourds peuvent être caractérisés par de très grandes vitesses et mettre en danger les aéronefs plus petits.  5, fiche 1, Français, - tourbillon%20en%20bout%20d%27aile

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tourbillon en bout d'aile; tourbillon d'extrémité d'aile : termes et définition normalisés par le Comité sur le Glossaire à l'intention des pilotes et du personnel des services de la circulation aérienne.  6, fiche 1, Français, - tourbillon%20en%20bout%20d%27aile

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, Textual support number: 1 CONT

Embedded GPS INS. The EGI is in an all-attitude navigation system providing outputs of linear and angular acceleration, velocity, position, attitude(roll, pitch, and platform azimuth), magnetic and true heading, altitude, time tags, and time. When installed in the host platforms in the appropriate configuration, the system provides the navigation functions of the equipment it replaces. It uses vehicle electrical power(28 Vdc), turn-on and mode commands, initialization data, and altitude data, as well as Global Positioning System(GPS) satellite inputs for GPS or GPS/Inertial Navigation System(INS) operation, and is able to track five space vehicles simultaneously.  1, fiche 2, Anglais, - all%2Dattitude%20navigation%20system

Record number: 2, Textual support number: 1 OBS

Attitude. The angle between an imaginary line running from the nose to the tail, and the horizontal. The attitude is judged by the level at which the horizon is seen through the canopy.  4, fiche 2, Anglais, - all%2Dattitude%20navigation%20system

Fiche 2,  Justifications,  Français

Record number: 2, Textual support number: 1 CONT

GPS et INS intégrés. Le système EGI est un système de navigation toutes attitudes qui fournit un signal d'accélération linéaire et angulaire, de vitesse, de position, d'attitude (roulis, tangage et azimut de plate-forme), un cap magnétique et vrai, l'altitude, les descripteurs temps et l'heure. Lorsqu'il est installé dans les plates-formes hôtes sous sa configuration appropriée, le système fournit les fonctions de navigation de l'équipement qu'il remplace. Il utilise le courant électrique de l'aéronef (28 V CC), les commandements de mise en marche et de mode, les données d'initialisation ainsi que les données d'altitude de même que les entrées satellites du système de positionnement global (GPS) pour le fonctionnement en GPS ou en GPS/système de navigation par inertie (INS) et peut poursuivre cinq véhicules spatiaux simultanément.  1, fiche 2, Français, - syst%C3%A8me%20de%20navigation%20toutes%20attitudes

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, Textual support number: 1 CONT

IRUs are self-contained systems comprised of gyros and accelerometers that provide aircraft altitude(pitch, roll, and heading), position, and velocity information in response to signals resulting from inertial effects on system components. Once aligned with a known position, IRUs continuously calculate position and velocity. IRU position accuracy decays with time.  2, fiche 3, Anglais, - inertial%20reference%20unit

Record number: 3, Textual support number: 1 OBS

inertial reference unit; IRU: term and abbreviation officially approved by the Air Force Terminology Panel (Trenton).  3, fiche 3, Anglais, - inertial%20reference%20unit

Fiche 3,  Justifications,  Français

Record number: 3, Textual support number: 1 OBS

centrale inertielle de référence; IRU : terme et abréviation uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et par le Groupe d'experts en terminologie de la Force aérienne (Trenton).  2, fiche 3, Français, - centrale%20inertielle%20de%20r%C3%A9f%C3%A9rence

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Record number: 4, Textual support number: 1 CONT

The gyros are used to maintain the platform’s inertial orientation by sensing rotations of the platform caused by vehicle-rotation-induced friction at the gimbal pivot points ... One gyro - called the vertical gyro - is oriented so its input axes are aligned with the X and Y platform axes; its input axes provide IMU [Inertial Measurement Unit] platform roll and pitch stabilization. The second gyro is oriented so that one input axis lies along the platform’s Z axis and the other lies in the X-Y plane. This gyro - the azimuth gyro - provides platform yaw stabilization with the Z input axis, while the second input axis is used as a platform rate detector for built-in test equipment.  3, fiche 4, Anglais, - azimuth%20gyroscope

Record number: 4, Textual support number: 2 CONT

The sensors for angular velocity are vibrating gyroscopes(3 axes, to detect rotation and pitch/roll pendulations of the payload). An error signal is obtained differencing the signal from the azimuth gyroscope and a constant level settable from the telemetry, which controls the speed of rotation. Such error signal drives an analog PID [Proportional Integral Differential] circuit; the output of the PID is connected to the PWM [Pulse Width Modulation] driver supplying current to the pivot azimuth motors.  3, fiche 4, Anglais, - azimuth%20gyroscope

Record number: 4, Textual support number: 3 CONT

azimuth gyro: term used at Natural Resources Canada - Earth Sciences Sector.  4, fiche 4, Anglais, - azimuth%20gyroscope

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Azimuth gyro drift rate.  5, fiche 4, Anglais, - azimuth%20gyroscope

Fiche 4,  Justifications,  Français

Record number: 4, Textual support number: 1 CONT

La plate-forme stabilisée [...] Trois gyroscopes sont utilisés : (a) Un gyroscope d'azimut qui, n'ayant aucun degré de liberté dans l'axe vertical, détecte tout déplacement de la plate-forme en azimut. (b) Deux gyroscopes d'inclinaison [...]  3, fiche 4, Français, - gyroscope%20d%27azimut

Record number: 4, Textual support number: 1 OBS

gyroscope d'azimut : terme en usage à Ressources naturelles Canada - Secteur des sciences de la Terre.  4, fiche 4, Français, - gyroscope%20d%27azimut

Record number: 4, Textual support number: 1 PHR

Vitesse de dérive du gyroscope d'azimut.  5, fiche 4, Français, - gyroscope%20d%27azimut

Fiche 4,  Justifications,  Espagnol

Fiche 5,  Justifications,  Anglais

Record number: 5, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : Vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, fiche 5, Anglais, - roll%20axis

Record number: 5, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation: roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle’s centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight. ... The axes of a cylindrical spacecraft (e.g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft (i.e. defined relative to the pilot’s seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc": the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth’s spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  4, fiche 5, Anglais, - roll%20axis

Record number: 5, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  4, fiche 5, Anglais, - roll%20axis

Record number: 5, Textual support number: 2 OBS

roll axis; axis of roll: terms officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  5, fiche 5, Anglais, - roll%20axis

Fiche 5,  Justifications,  Français

Record number: 5, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  1, fiche 5, Français, - axe%20de%20roulis

Record number: 5, Textual support number: 1 OBS

axe de roulis : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, fiche 5, Français, - axe%20de%20roulis

Fiche 5,  Justifications,  Espagnol

Fiche 6,  Justifications,  Anglais

Record number: 6, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : Vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  2, fiche 6, Anglais, - pitch%20axis

Record number: 6, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation: roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle’s centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight. ... The axes of a cylindrical spacecraft (e.g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft (i.e. defined relative to the pilot’s seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc": the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth’s spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  3, fiche 6, Anglais, - pitch%20axis

Record number: 6, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  3, fiche 6, Anglais, - pitch%20axis

Record number: 6, Textual support number: 2 OBS

pitch axis: term officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, fiche 6, Anglais, - pitch%20axis

Fiche 6,  Justifications,  Français

Record number: 6, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  2, fiche 6, Français, - axe%20de%20tangage

Record number: 6, Textual support number: 1 OBS

axe de tangage : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2.  3, fiche 6, Français, - axe%20de%20tangage

Fiche 6,  Justifications,  Espagnol

Fiche 7,  Justifications,  Anglais

Record number: 7, Textual support number: 1 DEF

The rotation of a vehicle about its vertical (Z) axis, i.e. movement in azimuth.  2, fiche 7, Anglais, - yaw

Record number: 7, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, fiche 7, Anglais, - yaw

Record number: 7, Textual support number: 1 OBS

yaw: term officially approved by the International Space Station Official Approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, fiche 7, Anglais, - yaw

Fiche 7,  Justifications,  Français

Record number: 7, Textual support number: 1 DEF

Mouvement d'un corps autour d'un axe perpendiculaire aux axes de roulis et de tangage.  2, fiche 7, Français, - lacet

Record number: 7, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  3, fiche 7, Français, - lacet

Record number: 7, Textual support number: 1 OBS

lacet : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  4, fiche 7, Français, - lacet

Fiche 7,  Justifications,  Espagnol

Fiche 8,  Justifications,  Anglais

Record number: 8, Textual support number: 1 CONT

Preprocessing is an important and diverse set of image preparation programs that act to offset problems with the band data and recalculate DN [Digital Number] values that minimize these problems. Among the programs that optimize these values are atmospheric correction(affecting the DNs of surface materials because of radiance from the atmosphere itself, involving attenuation and scattering) ;Sun illumination geometry; surface-induced geometric distortions; spacecraft velocity and attitude variations(roll, pitch, and yaw) ;effects of Earth rotation, elevation, curvature(including skew effects), abnormalities of instrument performance(irregularities of detector response and scan mode such as variations in mirror oscillations) ;loss of specific scan lines(requires destriping), and others. Once performed on the raw data, these adjustments require appropriate radiometric and geometric corrections.  2, fiche 8, Anglais, - preprocessing

Record number: 8, Textual support number: 1 OBS

preprocessing: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  3, fiche 8, Anglais, - preprocessing

Fiche 8,  Justifications,  Français

Record number: 8, Textual support number: 1 CONT

La première étape de prétraitement des données SAR correspond à la transformation des données 16 bits en données 8 bits et ce, afin de faciliter la manipulation ainsi que la combinaison avec les autres données optiques qui sont, généralement, sur 8 bits. La deuxième étape consiste à réduire le châtoiement inhérent aux images SAR [radar à synthèse d'ouverture] [...] La troisième étape comprend le prétraitement des données TM [Thematic Mapper] de Lansat dont le but vise essentiellement l'amélioration de la qualité des images. Cette étape est effectuée en trois phases : la superposition géométrique, le géocodage des images optiques comparées à une image SAR disponible de type GEC [Geocoded Ellipsoid Corrected] et, enfin, le rééchantillonnage des pixels à une résolution de 25 m.  2, fiche 8, Français, - pr%C3%A9traitement

Record number: 8, Textual support number: 1 OBS

prétraitement : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  3, fiche 8, Français, - pr%C3%A9traitement

Fiche 8,  Justifications,  Espagnol

Fiche 9,  Justifications,  Anglais

Record number: 9, Textual support number: 1 OBS

Embedded GPS INS. The EGI is in an all-attitude navigation system providing outputs of linear and angular acceleration, velocity, position, attitude(roll, pitch, and platform azimuth), magnetic and true heading, altitude, time tags, and time. When installed in the host platforms in the appropriate configuration, the system provides the navigation functions of the equipment it replaces.  2, fiche 9, Anglais, - all%2Dattitude%20platform

Fiche 9,  Justifications,  Français

Record number: 9, Textual support number: 1 OBS

GPS et INS intégrés. Le système EGI est un système de navigation toutes attitudes qui fournit un signal d'accélération linéaire et angulaire, de vitesse, de position, d'attitude (roulis, tangage et azimut de plate-forme), un cap magnétique et vrai, l'altitude, les descripteurs temps et l'heure. Lorsqu'il est installé dans les plates-formes hôtes sous sa configuration appropriée, le système fournit les fonctions de navigation de l'équipement qu'il remplace.  2, fiche 9, Français, - plate%2Dforme%20gyroscopique%20toutes%20attitudes

Record number: 9, Textual support number: 2 OBS

Pluriel : des plateformes, des plates-formes.  3, fiche 9, Français, - plate%2Dforme%20gyroscopique%20toutes%20attitudes

Record number: 9, Textual support number: 3 OBS

plateforme (sing.); plateformes (pl.) : Ces graphies, puisées des Rectifications de l'orthographe recommandées par le Conseil supérieur de la langue française, sont attestées dans le Petit Robert (2004).  4, fiche 9, Français, - plate%2Dforme%20gyroscopique%20toutes%20attitudes

Fiche 9,  Justifications,  Espagnol

Fiche 10,  Justifications,  Anglais

Record number: 10, Textual support number: 1 CONT

The Attitude and Vernier Upper Module. The Vega launch vehicle is equipped with a liquid propulsion module(AVUM), which provides roll control and pitch, yaw, and axial thrust during the final phase of flight. It shall perform the following functions :-roll control;-attitude control during coasting flight and in orbit phase;-correction of axial velocity error due to solid rocket motor performance scatter;-generation of the required velocity change for orbit circularisation(as required) ;-satellite pointing;-satellite release manoeuvres;-empty stage de-orbiting.  2, fiche 10, Anglais, - attitude%20and%20Vernier%20upper%20module

Fiche 10,  Justifications,  Français

Record number: 10, Textual support number: 1 CONT

Enfin, on attend la signature du contrat de développement du petit lanceur Vega. Il s'agit d'un lanceur composé de trois étages à propergol solide, surmonté d'un module supérieur à liquide dit AVUM (Attitude and Vernier Upper Module) - permettant le contrôle d'attitude et d'orbite, la séparation des satellites et la désorbitisation - ainsi que d'une coiffe.  2, fiche 10, Français, - module%20sup%C3%A9rieur%20Vernier%2Fcommande%20d%27orientation

Fiche 10,  Justifications,  Espagnol

Fiche 11,  Justifications,  Anglais

Record number: 11, Textual support number: 1 CONT

The description of the Station's flight attitude(orientation relative to the plane of its orbit) is referenced to local-vertical/local-horizontal(LVLH) axes that are fixed with respect to the Station's near-circular orbit(i. e., not to the physical Station). The LVLH origin is at the Station's center-of-mass; the z-axis points radially toward the Earth's center(or toward the nadir direction), the x-axis points along the orbital velocity vector(the ram direction, with wake being opposite), and the y-axis completes the right-handed triad. The flight attitude of the Station is then described using a second, Station-fixed, coordinate system whose orientation relative to LVLH is specified using the Eulerian angles of yaw, pitch and roll. Several Station-fixed coordination systems are defined. The most widely used is the Space Station Reference Coordinate System,... in thich the positive x-axis points along the axis of the U. S. lab away from the Zarya and Service Modules; the positive y-axis points starboard along the main truss, and positive z completes a right-handed coordinate system.  2, fiche 11, Anglais, - Station%27s%20flight%20attitude

Record number: 11, Textual support number: 1 OBS

Station’s flight attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, fiche 11, Anglais, - Station%27s%20flight%20attitude

Fiche 11,  Justifications,  Français

Record number: 11, Textual support number: 1 CONT

Iouri Onoufrienko et Dan Bursch, qui avaient enfilé des combinaisons spatiales russes Orlan, ont installé six écrans de protection autour des micropropulseurs qui servent à contrôler l'attitude de la Station et qui sont situés à l'arrière du module Zvezda.  3, fiche 11, Français, - attitude%20de%20la%20Station

Record number: 11, Textual support number: 1 OBS

attitude de la Station : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  4, fiche 11, Français, - attitude%20de%20la%20Station

Fiche 11,  Justifications,  Espagnol

Fiche 12,  Justifications,  Anglais

Record number: 12, Textual support number: 1 CONT

Shear layers can be made unstable so that they fluctuate and roll up into discrete vortical structures. The shape of the velocity profile is the key to determining stability.  2, fiche 12, Anglais, - shear%20layer

Record number: 12, Textual support number: 1 PHR

Shear layer equation.  3, fiche 12, Anglais, - shear%20layer

Fiche 12,  Justifications,  Français

Record number: 12, Textual support number: 1 CONT

On veut étudier à l'aide de Fluent une zone de mélange (zone de cisaillement entre deux fluides animés de deux vitesses différentes). Cet écoulement a été étudié en cours de turbulence dans le cadre des écoulements cisaillés plans.  3, fiche 12, Français, - zone%20de%20m%C3%A9lange

Fiche 12,  Justifications,  Espagnol

Fiche 13,  Justifications,  Anglais

Record number: 13, Textual support number: 1 DEF

Surface-wave energy which travels along or near the surface of the ground. Usually characterized by relatively low velocity and low frequency but high amplitude. Ground roll tends to mask desired signals.  3, fiche 13, Anglais, - ground%2Droll

Fiche 13,  Justifications,  Français

Record number: 13, Textual support number: 1 DEF

Onde superficielle provoquée par les tirs sismiques et perturbant les enregistrements.  2, fiche 13, Français, - ground%2Droll

Record number: 13, Textual support number: 1 CONT

Le bruit sismique comprend les parasites dus aux ondes de surface et aux ondes transversales (ground-roll).  3, fiche 13, Français, - ground%2Droll

Record number: 13, Textual support number: 1 OBS

On pense que les ondes de Rayleigh constituent le principal composant du ground-roll.  1, fiche 13, Français, - ground%2Droll

Fiche 13,  Justifications,  Espagnol

Fiche 14,  Justifications,  Anglais

Record number: 14, Textual support number: 1 CONT

(...) design studies on the dynamic response of the aircraft have led us to cover the effects at touchdown of many parameters(...) These included bank angle, rate of roll, inward and outward sideslip velocity(...)  1, fiche 14, Anglais, - outward%20sideslip%20velocity

Fiche 14,  Justifications,  Français

Record number: 14, Textual support number: 1 OBS

Renseignement fourni par Joël Larue, traducteur, Technique centrale III.  1, fiche 14, Français, - vitesse%20de%20d%C3%A9rapage

Fiche 14,  Justifications,  Espagnol

Fiche 15,  Justifications,  Anglais

Record number: 15, Textual support number: 1 CONT

(...) design studies on the dynamic response of the aircraft have led us to cover the effects of many parameters(...) These included bank angle, rate of roll, inward and outward sideslip velocity(...)  1, fiche 15, Anglais, - inward%20sideslip%20velocity

Record number: 15, Textual support number: 1 OBS

sideslip: to slide side ways through the air in the downward direction along an inclined lateral axis esp. to slide in such a manner while turning.  2, fiche 15, Anglais, - inward%20sideslip%20velocity

Fiche 15,  Justifications,  Français

Record number: 15, Textual support number: 1 OBS

Renseignement fourni par Joël Larue, traducteur, Technique centrale III.  1, fiche 15, Français, - vitesse%20de%20glissade

Fiche 15,  Justifications,  Espagnol

Fiche 16,  Justifications,  Anglais

Record number: 16, Textual support number: 1 CONT

Experience with the P. 1127... has proved that unautostabilised hovering is easier than with many helicopters, since the P. 1127 types... are virtually unaffected by gusts, due to the low ratio of gust/jet velocity.... the Harrier is provided with limited authority autostabilisation in roll and pitch, to facilitate control under difficult weather conditions and at night.  1, fiche 16, Anglais, - limited%20authority%20autostabilisation

Fiche 16,  Justifications,  Français

Fiche 16,  Justifications,  Espagnol