TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

... the valves, on command from the directional control electronics, inject fuel into the booster exhaust stream, creating side forces that change the direction of the main thrust vector, thus changing the missile's pitch or yaw axis.  1, record 1, English, - booster%20exhaust%20stream

Record 1,  Textual support,  French

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

The default pitch axis mode is pitch hold(PIT). When no other pitch axis modes are selected, this is the active pitch axis mode when the autopilot and/or flight director is engaged.  2, record 2, English, - pitch%20axis%20command%20mode

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

mode directive de tangage : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  2, record 2, French, - mode%20directive%20de%20tangage

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

The elevator trim tab control system incorporates an autopilot servomotor. This system provides automatic trimming of the aircraft in the pitch axis.  3, record 3, English, - autopilot%20servo

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

servo pilote automatique : terme uniformisé par le Comité d’uniformisation de la terminologie aéronautique (CUTA) – Opérations aériennes.  5, record 3, French, - servomoteur%20du%20pilote%20automatique

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 DEF

A propeller system that allows the pilot to adjust the pitch during flight by means of a hydraulic mechanism.  3, record 4, English, - variable%2Dpitch%20propeller

Record number: 4, Textual support number: 1 CONT

The blades of a variable-pitch propeller are attached to a mechanism in the hub that rotates the entire blade about an axis that runs along the length of the blade … This allows the blade pitch to be varied continuously by the pilot to maintain optimum efficiency at any airspeed.  4, record 4, English, - variable%2Dpitch%20propeller

Record number: 4, Textual support number: 1 OBS

Variable-pitch propellers include propellers whose pitch can be set up automatically and propellers whose pitch can be set up manually (i.e. by pilot’s operation). Although "controllable-pitch propeller" can be a synonym of "variable-pitch propeller," most authors consider that controllable-pitch propellers only include propellers whose pitch can be changed manually.  5, record 4, English, - variable%2Dpitch%20propeller

Record number: 4, Textual support number: 2 OBS

controllable-pitch propeller: term standardized by the British Standards Institution.  6, record 4, English, - variable%2Dpitch%20propeller

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 DEF

Hélice dont on peut régler le pas de façon à modifier le couple résistant.  3, record 4, French, - h%C3%A9lice%20%C3%A0%20pas%20variable

Record number: 4, Textual support number: 1 CONT

Au début, les hélices étaient à pales fixes, réglées pour la vitesse maximale, et ayant un très mauvais rendement au décollage, où une grande puissance est nécessaire. Aujourd'hui, on n'emploie plus que des hélices à pas variable. Dans ces hélices, les pales peuvent tourner autour de leur axe longitudinal (perpendiculaire à l'arbre moteur) pour prendre une inclinaison variable; elles sont actionnées par un moteur électrique ou un piston hydraulique par l'intermédiaire d'un système de leviers ou d'engrenages et de crémaillères, le tout situé dans le carter de l'hélice. L'inclinaison peut être commandée soit à la main, soit automatiquement en fonction de la vitesse du moteur et de la résistance de l'air sur les pales, de manière que le rendement soit toujours optimal.  4, record 4, French, - h%C3%A9lice%20%C3%A0%20pas%20variable

Record 4,  Textual support,  Spanish

Record number: 4, Textual support number: 1 CONT

Para obtener el mejor rendimiento del motor en condiciones de vuelo muy diferentes (despegue, crucero, vuelo bajo o estratosférico, etc.) se usan hélices de paso variable donde el ángulo de ataque es modificado en el curso del vuelo ya por el piloto, ya por un dispositivo automático.  2, record 4, Spanish, - h%C3%A9lice%20de%20paso%20variable

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

In other small machines the centrifugal force on the blades as the rotational speed rises, is made to change their pitch. The blade fixing at the hub may have a spiral socket so that the blades changes pitch as i is pulled radially outwards by this force or, alternatively, the blade spindle may be bent near the hub so that the centre of gravity of the blade lies off the axis of rotation. Pitch changing with a fly-ball governor is used in the small Winpower machines.  1, record 5, English, - pitch%20changing

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 CONT

Régulation. Principe (...) : variation du calage des pales commandée par des masselottes centrifuges comprimant des ressorts, ce qui a pour effet de faire basculer l'effort aérodynamique dont la composante dans le plan de rotation de l'hélice devient résistante.  1, record 5, French, - variation%20du%20calage

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 DEF

The movement or an aircraft about the vertical axis.  4, record 6, English, - yaw%20axis

Record number: 6, Textual support number: 1 CONT

The aircraft can rotate around three axes : the fore-and-aft axis(or the roll axis) ;the span-wise(nose-up/nose-down) axis or the pitch axis; and the nose-left/nose-right, or yaw axis.  5, record 6, English, - yaw%20axis

Record number: 6, Textual support number: 1 OBS

yaw axis: term officially approved by the International Civil Aviation Organization (ICAO).  3, record 6, English, - yaw%20axis

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 DEF

Axe perpendiculaire aux axes de roulis et de tangage.  2, record 6, French, - axe%20de%20lacet

Record number: 6, Textual support number: 1 CONT

[...] il effectue aussi des rotations autour des trois axes liés à la machine : axe de roulis (ou axe longitudinal, basculer droite/gauche), axe de tangage (axe transversal, piqué/cabré) et axe de lacet (axe vertical, rotation droite/gauche). Tous ces déplacements et rotations étant combinables, on imagine que toutes les trajectoires et attitudes instantanées sont possibles sous l'action d'un pilote expérimenté.  3, record 6, French, - axe%20de%20lacet

Record number: 6, Textual support number: 1 OBS

axe de lacet : terme uniformisé par l'Organisation de l'aviation civile internationale (OACI); les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  4, record 6, French, - axe%20de%20lacet

Record 6,  Textual support,  Spanish

Record number: 6, Textual support number: 1 OBS

eje de guiñada: término aceptado oficialmente por la Organización de Aviación Civil Internacional (OACI).  2, record 6, Spanish, - eje%20de%20gui%C3%B1ada

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 DEF

The axis which runs from wing tip to wing tip through the centre of gravity.  3, record 7, English, - pitch%20axis

Record number: 7, Textual support number: 1 CONT

The pitch axis is perpendicular to the aircraft centerline and lies in the plane of the wings. A pitch motion is an up or down movement of the nose of the aircraft... The pitching motion is being caused by the deflection of the elevator of this aircraft. The elevator is a hinged section at the rear of the horizontal stabilizer. There is usually an elevator on each side of the vertical stabilizer. The elevators work in pairs; when the right elevator goes up, the left elevator also goes up.  4, record 7, English, - pitch%20axis

Record number: 7, Textual support number: 2 CONT

The aircraft can rotate around three axes : the fore-and-aft axis(or the roll axis) ;the span-wise(nose-up/nose-down) axis or the pitch axis; and the nose-left/nose-right, or yaw axis.  5, record 7, English, - pitch%20axis

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 DEF

Mouvement de l'avion contrôlé par la gouverne de profondeur.  2, record 7, French, - axe%20de%20tangage

Record number: 7, Textual support number: 1 CONT

La centrale d'attitude et de cap peut être à cardans ou à composants liés [...] et utiliser des gyroscopes mécaniques ou des gyrolasers. Dans le cas d'une centrale à cardans par exemple : un gyroscope à deux axes sensibles maintient la direction de la verticale vraie et matérialise ainsi la position de la ligne d'horizon par rapport aux axes de roulis et de tangage de l'avion, c'est-à-dire ses assiettes; un gyroscope à un axe sensible est utilisé pour maintenir un cap directionnel ou gyromagnétique.  3, record 7, French, - axe%20de%20tangage

Record number: 7, Textual support number: 2 CONT

La gouverne de profondeur est un volet mobile situé sur l'arrière de l'empennage horizontal, qui lui-même est placé vers la queue de l'appareil. En modifiant l'angle de la gouverne de profondeur, le pilote modifie la force agissant sur l'empennage horizontal et, grâce à un bras de levier important, cette variation de force fait piquer ou cabrer l'avion autour de l'axe de tangage, axe horizontal passant par le centre de gravité de l'avion. Cette commande permet de régler l'incidence de l'avion.  4, record 7, French, - axe%20de%20tangage

Record number: 7, Textual support number: 1 OBS

axe de tangage : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  5, record 7, French, - axe%20de%20tangage

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 DEF

[A horizontal axis wind turbine] where the global pitch angle [of the blades] does not change dynamically...  7, record 8, English, - fixed%2Dpitch%20wind%20turbine

Record number: 8, Textual support number: 1 CONT

Pitch Regulation. Once the rated wind speed has been reached, a WT [wind turbine] will be unable to make use of all of the wind energy incident on the rotor plane and must shed some. A pitch-regulated WT [wind turbine] will do this [namely] by pitching the blades to increase the angle of attack to cause sections of the blade to stall (in pitch-to-stall machines).  4, record 8, English, - fixed%2Dpitch%20wind%20turbine

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 DEF

Éolienne à axe horizontal dont le rotor est muni de pales fixées de manière rigide au moyeu et qui est régulée soit par effacement du rotor, soit par décrochage aérodynamique passif des pales.  4, record 8, French, - %C3%A9olienne%20%C3%A0%20pas%20fixe

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 DEF

The turn rate of 3° per second normally used by aircraft operating at less than 250 kt [knots].  6, record 9, English, - standard%20rate%20turn

Record number: 9, Textual support number: 1 CONT

The attitude indicator shows rotation about both the longitudinal axis to indicate the degree of bank, and about the lateral axis to indicate pitch(nose up, level or nose down)... The principal parts of interest to the pilot are : The miniature wings attached to the case remain parallel to the wings of the aircraft. The horizon bar which separates the top(light) and bottom(dark) halves to the ball. The degree marks on the upper periphery of the dial. The first 3 on both sides of center are 10 degrees apart, then 60 degree bank marks, and 90 degree bank marks. Fifteen degrees of bank is called a standard rate turn.  7, record 9, English, - standard%20rate%20turn

Record number: 9, Textual support number: 2 CONT

The turn indicator indicates the rate of the turn, not the amount of the turn. Thus a standard rate, or rate one, turn will give a rate of turn of 3 degrees per second, or 360 degrees in two minutes.  8, record 9, English, - standard%20rate%20turn

Record number: 9, Textual support number: 1 OBS

rate one turn: term and definition standardized by the Glossary for Pilots and Air Traffic Services Personnel Committee.  9, record 9, English, - standard%20rate%20turn

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 DEF

Taux de virage, de 3° par seconde, normalement utilisé par les aéronefs évoluant à moins de 250 kt [nœuds].  6, record 9, French, - virage%20%C3%A0%20taux%20standard

Record number: 9, Textual support number: 1 CONT

Virage à taux standard. Lorsque les ailes de l'avion miniature sont alignées avec les petits traits à côté de «G» (gauche) et «D» (droite), l'appareil effectue un virage à taux standard, soit 3 degrés par seconde pour le Cessna 182RG. Cela signifie que l'appareil accomplit un tour complet de 360 degrés en deux minutes.  7, record 9, French, - virage%20%C3%A0%20taux%20standard

Record number: 9, Textual support number: 2 CONT

L'indicateur de virage indique le taux de virage et non l'amplitude. Le taux standard, ou virage au taux 1, est égal à 3 degrés par seconde ou 360 degrés en deux minutes.  8, record 9, French, - virage%20%C3%A0%20taux%20standard

Record number: 9, Textual support number: 1 OBS

virage standard au taux un : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  9, record 9, French, - virage%20%C3%A0%20taux%20standard

Record number: 9, Textual support number: 2 OBS

virage de taux un : terme et définition normalisés par le Comité sur le Glossaire à l'intention des pilotes et du personnel des services de la circulation aérienne.  10, record 9, French, - virage%20%C3%A0%20taux%20standard

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 DEF

[A] gyro that tends to compensate the motion of aircraft with reference to the transverse(pitch) axis OY.  3, record 10, English, - pitch%20rate%20gyroscope

Record number: 10, Textual support number: 1 CONT

The gyropilot commonly called an automatic pilot ... The roll disturbance is detected by a roll rate gyroscope and by a roll angle pendulum, which senses displacement. The aileron servo applies corrective action. Pitch disturbance is detected by a pitch rate gyroscope and a pitch pendulum. The elevator servo applies corrective action.  1, record 10, English, - pitch%20rate%20gyroscope

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 OBS

Un gyromètre est un gyroscope qui ne possède qu'un seul cadre de suspension, c'est-à-dire un seul degré de liberté, et qui sert à mesurer une vitesse angulaire de rotation.  3, record 10, French, - gyrom%C3%A8tre%20de%20tangage

Record number: 10, Textual support number: 2 OBS

gyromètre de tangage : terme d'usage obligatoire au Bureau de la traduction du Canada.  4, record 10, French, - gyrom%C3%A8tre%20de%20tangage

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, 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, record 11, English, - azimuth%20gyroscope

Record number: 11, 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, record 11, English, - azimuth%20gyroscope

Record number: 11, Textual support number: 3 CONT

azimuth gyro: term used at Natural Resources Canada - Earth Sciences Sector.  4, record 11, English, - azimuth%20gyroscope

Record number: 11, Textual support number: 1 PHR

Azimuth gyro drift rate.  5, record 11, English, - azimuth%20gyroscope

Record 11,  Textual support,  French

Record number: 11, 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, record 11, French, - gyroscope%20d%27azimut

Record number: 11, Textual support number: 1 OBS

gyroscope d'azimut : terme en usage à Ressources naturelles Canada - Secteur des sciences de la Terre.  4, record 11, French, - gyroscope%20d%27azimut

Record number: 11, Textual support number: 1 PHR

Vitesse de dérive du gyroscope d'azimut.  5, record 11, French, - gyroscope%20d%27azimut

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 DEF

[A] two-degrees-of-freedom gyro torqued on gimbal mounts to hold spin axis vertical, thus giving output signals proportional to rotation about two orthogonal axes, usually pitch/roll.  7, record 12, English, - vertical%20gyroscope

Record number: 12, Textual support number: 1 CONT

A vertical gyro is a gyroscope whose spin axis is "stabilized" or gimbaled to remain vertical with respect to gravity. The vertical gyro is used to measure rotations away from vertical relative to the fixed earth reference frame.  8, record 12, English, - vertical%20gyroscope

Record number: 12, Textual support number: 1 OBS

In this gyro, output signals are produced by gimbal angular displacements that correspond to angular displacements of the case surrounding two nominally orthogonal, horizontal axes.  9, record 12, English, - vertical%20gyroscope

Record number: 12, Textual support number: 2 OBS

Attitude gyros, technically called vertical gyros because of the orientation of their spin axis ...  6, record 12, English, - vertical%20gyroscope

Record 12,  Textual support,  French

Record number: 12, Textual support number: 1 DEF

Instrument qui détecte les montées ou descentes de l'avion, ainsi que les inclinaisons à droite ou à gauche.  6, record 12, French, - gyroscope%20de%20verticale

Record number: 12, Textual support number: 1 CONT

Indicateur de verticale. C'est un appareil comportant un gyroscope dont le moment cinétique est dirigé au mieux suivant la verticale. Le carter du gyroscope est monté à la Cardan suivant les axes de roulis ou de tangage du bâtiment [...] Les pendules détecteurs (roulis ou tangage) détectent les écarts de verticale, et ils alimentent les moteurs couples correspondants (roulis ou tangage) de façon à ramener les signaux des pendules à zéro, le moment cinétique du gyroscope est ainsi maintenu vertical.  3, record 12, French, - gyroscope%20de%20verticale

Record number: 12, Textual support number: 1 OBS

[Cet instrument] surveille donc, dans le pilotage automatique, les mouvements de tangage et de roulis.  6, record 12, French, - gyroscope%20de%20verticale

Record number: 12, Textual support number: 2 OBS

gyro de verticale : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  7, record 12, French, - gyroscope%20de%20verticale

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 CONT

The roll axis lies along the aircraft centerline. A roll motion is an up and down movement of the wings of the aircraft ... The rolling motion is being caused by the deflection of the aileron of this aircraft. The aileron is a hinged section at the rear of each wing. The ailerons work in opposition; when the right aileron goes up, the left aileron goes down.  4, record 13, English, - roll%20axis

Record number: 13, Textual support number: 2 CONT

The aircraft can rotate around three axes : the fore-and-aft axis(or the roll axis) ;the span-wise(nose-up/nose-down) axis or the pitch axis; and the nose-left/nose-right, or yaw axis.  3, record 13, English, - roll%20axis

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 CONT

La centrale d'attitude et de cap peut être à cardans ou à composants liés [...] et utiliser des gyroscopes mécaniques ou des gyrolasers. Dans le cas d'une centrale à cardans par exemple : un gyroscope à deux axes sensibles maintient la direction de la verticale vraie et matérialise ainsi la position de la ligne d'horizon par rapport aux axes de roulis et de tangage de l'avion, c'est-à-dire ses assiettes; un gyroscope à un axe sensible est utilisé pour maintenir un cap directionnel ou gyromagnétique.  2, record 13, French, - axe%20de%20roulis

Record number: 13, Textual support number: 1 OBS

axe de roulis : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  3, record 13, French, - axe%20de%20roulis

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 CONT

The heading axis servo system functions in a manner similar to the pitch and roll axes. Differences exist in the servo follow-up circuitry and in the manner of the application of the command to the servo system.  1, record 14, English, - servo%20follow%2Dup%20circuitry

Record 14,  Textual support,  French

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 CONT

Stabilisation and orientation by inertial flywheels consists in accurately aligning the axes of three flywheels with the axes of reference(roll, pitch and yaw)... The spherical orienter... uses the principle of inertial reaction. It consists essentially of a floating sphere supported electrostatically, magnetically or by an air cushion. This sphere can thus turn freely about any axis, friction being negligible. If the stator... exercises a couple on the sphere, it responds to this stress by an equal and opposite reaction couple, until it has attained its limiting speed or rotation(saturation).  1, record 15, English, - spherical%20orienter

Record 15,  Textual support,  French

Record number: 15, Textual support number: 1 OBS

[...] le télescope spatial Hubble connaît [...] des ennuis mécaniques. Son système d'orientation dans l'espace, composé de six gyroscopes, semble moribond. Déjà, deux des gyroscopes sont hors service alors qu'un troisième serait sur le point de tomber en panne. Hubble a besoin d'au moins quatre gyroscopes pour s'orienter dans l'espace et poursuivre ses observations astronomiques.  2, record 15, French, - syst%C3%A8me%20d%27orientation%20gyroscopique

Record number: 15, Textual support number: 2 OBS

Un gyroscope est un disque ou, dans ce cas-ci, une sphère qui tourne sur un axe. Une fois en rotation, l'axe continuera toujours à pointer dans la même direction si aucune autre force ne vient altérer son mouvement.  3, record 15, French, - syst%C3%A8me%20d%27orientation%20gyroscopique

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 DEF

The attitude of an aircraft, rocket, or other flying vehicle, referred to the relationship between the longitudinal body axis and a chosen reference line or plane as seen from the side.  3, record 16, English, - pitch%20attitude

Record number: 16, Textual support number: 1 CONT

The attitude indicator shows rotation about both the longitudinal axis to indicate the degree of bank, and about the lateral axis to indicate pitch(nose up, level or nose down). It utilizes the rigidity characteristic of the gyro. It is gimbaled to permit rotation about the lateral axis indicating pitch attitude, and about the longitudinal axis to indicate roll attitude.  4, record 16, English, - pitch%20attitude

Record number: 16, Textual support number: 1 OBS

body attitude: term used for the B-767.  5, record 16, English, - pitch%20attitude

Record number: 16, Textual support number: 2 OBS

pitch attitude: term officially approved by the International Civil Aviation Organization (ICAO).  6, record 16, English, - pitch%20attitude

Record number: 16, Textual support number: 1 PHR

Constant pitch attitude.  7, record 16, English, - pitch%20attitude

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 CONT

L'assiette de votre avion, plus précisément l'assiette longitudinale, est grossièrement ce qui fait voler l'avion, et cette assiette se pilote par le ... manche, d'avant en arrière!  4, record 16, French, - assiette%20en%20tangage

Record number: 16, Textual support number: 2 CONT

Le lacet est le mouvement latéral du nez de l'avion. L'assiette longitudinale, c'est-à-dire la position du nez par rapport à l'horizontale, reste constante bien que l'avion pivote vers la gauche ou vers la droite. Le lacet est contrôlé par la dérive sur l'empennage de l'avion.  5, record 16, French, - assiette%20en%20tangage

Record number: 16, Textual support number: 3 CONT

Le rôle de l'horizon artificiel est de définir la verticale du lieu, c'est-à-dire de donner au pilote les références avions, l'assiette longitudinale et l'inclinaison latérale.  6, record 16, French, - assiette%20en%20tangage

Record number: 16, Textual support number: 1 OBS

assiette en tangage; assiette longitudinale : termes uniformisés par l'Organisation de l'aviation civile internationale (OACI) et par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  7, record 16, French, - assiette%20en%20tangage

Record number: 16, Textual support number: 1 PHR

Assiette longitudinale constante.  8, record 16, French, - assiette%20en%20tangage

Record 16,  Textual support,  Spanish

Record number: 16, Textual support number: 1 OBS

actitud en cabeceo : término aceptado oficialmente por la Organización de Aviación Civil Internacional (OACI).  2, record 16, Spanish, - actitud%20en%20cabeceo

Record 17,  Textual support,  English

Record number: 17, 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, record 17, English, - roll%20axis

Record number: 17, 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, record 17, English, - roll%20axis

Record number: 17, 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, record 17, English, - roll%20axis

Record number: 17, 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, record 17, English, - roll%20axis

Record 17,  Textual support,  French

Record number: 17, 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, record 17, French, - axe%20de%20roulis

Record number: 17, 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, record 17, French, - axe%20de%20roulis

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, 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, record 18, English, - pitch%20axis

Record number: 18, 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, record 18, English, - pitch%20axis

Record number: 18, 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, record 18, English, - pitch%20axis

Record number: 18, 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, record 18, English, - pitch%20axis

Record 18,  Textual support,  French

Record number: 18, 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, record 18, French, - axe%20de%20tangage

Record number: 18, 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, record 18, French, - axe%20de%20tangage

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, Textual support number: 1 DEF

The angle between the axis and the pitch cone generator which contains the root cone generator.  1, record 19, English, - pitch%20angle

Record number: 19, Textual support number: 1 OBS

pitch angle: term and definition standardized by ISO.  2, record 19, English, - pitch%20angle

Record 19,  Textual support,  French

Record number: 19, Textual support number: 1 DEF

Angle entre l'axe et la génératrice du cône primitif de fonctionnement contenant la génératrice du cône de pied.  1, record 19, French, - angle%20primitif%20de%20fonctionnement

Record number: 19, Textual support number: 1 OBS

angle primitif de fonctionnement : terme et définition normalisés par l'ISO.  2, record 19, French, - angle%20primitif%20de%20fonctionnement

Record 19,  Textual support,  Spanish

Record 20,  Textual support,  English

Record number: 20, Textual support number: 1 DEF

A blade-to-rotor hub coupling that permits movement in and out of plane and about the pitch axis.  1, record 20, English, - delta%2D3%20blade%20hinge

Record 20,  Textual support,  French

Record number: 20, Textual support number: 1 DEF

Articulation pour moyeu de rotor éolien et de ses pales qui permet un mouvement de celles-ci à l'intérieur et hors du plan de rotation de même qu'autour de l'axe de tangage.  1, record 20, French, - articulation%20de%20pales%20delta%2D3

Record 20,  Textual support,  Spanish

Record 21,  Textual support,  English

Record number: 21, Textual support number: 1 DEF

The rotation of a vehicle about its vertical (Z) axis, i.e. movement in azimuth.  2, record 21, English, - yaw

Record number: 21, 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, record 21, English, - yaw

Record number: 21, 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, record 21, English, - yaw

Record 21,  Textual support,  French

Record number: 21, Textual support number: 1 DEF

Mouvement d'un corps autour d'un axe perpendiculaire aux axes de roulis et de tangage.  2, record 21, French, - lacet

Record number: 21, 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, record 21, French, - lacet

Record number: 21, 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, record 21, French, - lacet

Record 21,  Textual support,  Spanish

Record 22,  Textual support,  English

Record number: 22, Textual support number: 1 DEF

In contrast to full-span pitch control, where the rotation of a wind turbine blade about its longitudinal axis acts along its entire length, [a system where] only the outboard sections of the blade are used.  2, record 22, English, - partial%2Dspan%20pitch%20control

Record number: 22, Textual support number: 1 OBS

The inboard sections remain fixed in pitch.  2, record 22, English, - partial%2Dspan%20pitch%20control

Record 22,  Textual support,  French

Record number: 22, Textual support number: 1 DEF

À l'opposé du pas variable à rotation complète, où toute la pale d'une éolienne est sollicitée autour de son axe longitudinal, système qui ne fait appel qu'aux parties extérieures (arrière) de la pale, les parties intérieures demeurant fixes.  1, record 22, French, - commande%20de%20pas%20variable%20%C3%A0%20rotation%20partielle

Record number: 22, Textual support number: 1 OBS

Équivalent formulé après consultation du groupe ATI - Éolien division de Audace Technologies Inc. de Rimouski.  1, record 22, French, - commande%20de%20pas%20variable%20%C3%A0%20rotation%20partielle

Record 22,  Textual support,  Spanish

Record 23,  Textual support,  English

Record number: 23, Textual support number: 1 DEF

The mechanical axis formed by the wind turbine pitch articulation system(when it is supplied with the rotor blade).  2, record 23, English, - blade%20pitch%20axis

Record 23,  Textual support,  French

Record number: 23, Textual support number: 1 DEF

Axe mécanique du dispositif d'articulation de pas (si la pale [du rotor d'éolienne] en est munie).  1, record 23, French, - axe%20de%20pas

Record 23,  Textual support,  Spanish

Record 24,  Textual support,  English

Record number: 24, Textual support number: 1 DEF

A linear imperfection in a crystalline array of atoms.  2, record 24, English, - dislocation

Record number: 24, Textual support number: 1 CONT

Two basic types are recognized :(1) an edge dislocation corresponds to the row of mismatched atoms along the edge formed by an extra, partial plane of atoms within the body of a crystal;(2) a screw dislocation corresponds to the axis of a spiral structure in a crystal, characterized by a distortion that joins normally parallel planes together to form a continuous helical ramp(with a pitch of one interplanar distance) winding about the dislocaion. Most prevalent is the so-called mixed dislocation, which is any combination of an edge dislocation and a screw dislocation.  2, record 24, English, - dislocation

Record 24,  Textual support,  French

Record number: 24, Textual support number: 1 DEF

Défaut linéaire dans l'empilement atomique d'un cristal  2, record 24, French, - dislocation

Record number: 24, Textual support number: 1 CONT

Deux types principaux de dislocations sont définis : la dislocation «coin» et la dislocation «vis». La dislocation coin correspond à l'insertion d'un demi-plan supplémentaire d'atomes dans un cristal. Le bord intérieur de ce demi-plan définit la ligne de dislocation. Le déplacement des atomes consécutif à cette introduction est principalement orienté perpendiculairement à la ligne de dislocation. La dislocation vis correspond à une distorsion locale qui amène les plans atomiques à se raccorder en forme de rampe hélicoïdale s'enroulant autour d'un axe, la ligne de dislocation. Le pas de cette rampe est égal à une distance interatomique dans la direction de la ligne de dislocation. D'autres types de dislocations existent, résultats de l'association des deux types principaux définis ci-dessus. On distingue également les dislocations dissociées en partielles.  2, record 24, French, - dislocation

Record 24,  Textual support,  Spanish

Record 25,  Textual support,  English

Record number: 25, Textual support number: 1 CONT

For example, a one ounce imbalance 2 inches from the rotation axis causing a force of 21 lbs. But a Sensenich fixed pitch propeller on a small aircraft, such as the Piper Pacer, generates 13 tons of centrifugal stress per blade at its rated rpm of 2600.  1, record 25, English, - centrifugal%20stress

Record 25,  Textual support,  French

Record number: 25, Textual support number: 1 CONT

Hypothèse : On va tout d'abord simplifier la géométrie de l'hélice pour ramener son volume à un parallélépipède aux dimensions suivantes 4x300x2500. On peut ensuite évaluer les différentes contraintes s'appliquant à la pale. On distingue notamment la contrainte due à la force aérodynamique et la contrainte due à la force centrifuge.  1, record 25, French, - contrainte%20due%20%C3%A0%20la%20force%20centrifuge

Record 25,  Textual support,  Spanish

Record 26,  Textual support,  English

Record number: 26, Textual support number: 1 CONT

The ISS attitude will vary between +15 degrees and-15 degrees for each roll and yaw axis of LVLH [Local Vertical/Local Horizontal] and between +15 degrees to-20 degrees for the pitch axis... At any point on the ISS non-articulated portion, which means the portion excluding rotating elements such as photovoltaic arrays and Thermal Control System(TCS) radiators, the ISS will provide estimates of the ISS LVLH attitude to an accuracy of 3 degrees per axis(3 sigma) and inertial rates to an accuracy of 0. 01 degrees per second per axis(3 sigma). When controlling to the TEA [Torque Equilibrium Attitude] with non-propulsive effectors, the ISS will maintain attitude stability to 3. 5 degrees per axis per orbit.  2, record 26, English, - ISS%20attitude

Record number: 26, Textual support number: 1 OBS

ISS attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 26, English, - ISS%20attitude

Record 26,  Textual support,  French

Record number: 26, Textual support number: 1 OBS

attitude de la Station spatiale : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 26, French, - attitude%20de%20la%20Station%20spatiale

Record 26,  Textual support,  Spanish

Record 27,  Textual support,  English

Record number: 27, Textual support number: 1 DEF

The ability of a blade to turn on its longitudinal axis changing the pitch angle.  1, record 27, English, - feathering

Record 27,  Textual support,  French

Record number: 27, Textual support number: 1 DEF

Mouvement de rotation alterné d'une pale sur son axe longitudinal, par lequel le pas varie constamment.  1, record 27, French, - oscillation

Record 27,  Textual support,  Spanish

Record 28,  Textual support,  English

Record number: 28, Textual support number: 1 DEF

That action which changes the pitch angle of the rotor blades periodically by rotating them around their feathering(spanwise) axis.  1, record 28, English, - feathering%20action

Record 28,  Textual support,  French

Record number: 28, Textual support number: 1 DEF

Action changeant l'angle de pas des pales du rotor périodiquement en les faisant tourner autour de leur axe de changement de pas.  1, record 28, French, - action%20de%20changement%20de%20pas

Record 28,  Textual support,  Spanish

Record 29,  Textual support,  English

Record number: 29, Textual support number: 1 CONT

Controlled gyroscopes fall into three categories : north-seeking, directional, and gyrovertical. The north-seeking gyro is used for marine gyrocompasses... The directional gyroscope is used in aircraft and is sometimes called a self-levelling free gyroscope corrected for drift... The gyrovertical has its spin axis vertical and is used to detect and measure angles of roll and pitch.  1, record 29, English, - controlled%20gyroscope

Record number: 29, Textual support number: 1 OBS

A free gyro that is not slaved to any Earth reference (as the vertical and directional gyros and the gyrocompass are) will tend to maintain a fixed direction in inertial space, that is, with respect to fixed stars.  3, record 29, English, - controlled%20gyroscope

Record 29,  Textual support,  French

Record number: 29, Textual support number: 1 CONT

L'horizon artificiel. Il mesure simultanément une assiette et une inclinaison. L'utilisation d'un gyroscope asservi à la verticale lui permet de mesurer les angles compris entre l'axe du gyroscope et les axes liés à l'avion.  3, record 29, French, - gyroscope%20asservi

Record 29,  Textual support,  Spanish

Record 30,  Textual support,  English

Record number: 30, Textual support number: 1 CONT

The on-orbit Attitude Determination and Control Subsystem(ADACS) provides three axis pointing control for the satellite. The ADACS maintains system pointing by controlling torque in three mutually orthogonal wheels. The torque is determined by analysis of spacecraft orientation in space. Input to these computations are acquired from the Earth Sensor Assembly(ESA) for pitch and roll, and an inertial reference with sun sensor updates for yaw.  2, record 30, English, - inertial%20reference

Record 30,  Textual support,  French

Record number: 30, Textual support number: 1 CONT

Ce chapitre concerne l'étude fine d'un gyroscope [...], monté à 3 degrés de liberté [...] grâce à 2 armatures de Cardan. L'appareil est «le passager» d'une plate-forme stabilisée [...], d'orientation fixe dans un repère inertiel. I Description du montage : 1°) La plate-forme : [...] est un solide [...], emporté dans un véhicule (avion, sous marin, lanceur etc...), et conservant une orientation fixe par rapport à un repère inertiel. Ce qui ne veut pas dire que [la plate-forme stabilisée] est en translation uniforme, simplement en translation quelconque, avec accélération et vitesse.  3, record 30, French, - r%C3%A9f%C3%A9rence%20inertielle

Record number: 30, Textual support number: 2 CONT

Équipement de navigation. Ce type d'équipement guide l'aéronef vers son lieu de destination et intègre de nombreux produits tels que les systèmes de positionnement mondial [(...] GPS), la centrale anémobarométrique, qui calcule la vitesse aérodynamique, l'altitude et la vitesse verticale de l'appareil, les IRS («Inertial Reference System» - systèmes de référence inertielle) - qui sont les principaux capteurs de mouvement et de navigation de la cellule utilisés par un nombre très élevé de systèmes avioniques [...]  4, record 30, French, - r%C3%A9f%C3%A9rence%20inertielle

Record 30,  Textual support,  Spanish

Record 31,  Textual support,  English

Record number: 31, Textual support number: 1 CONT

The main AI [attitude indicator] used an electrically driven, two axis of freedom, vertical gyroscope assembly... Attitude information was displayed by a sphere which was mechanically driven by the pitch gimbal and directly attached to the roll gimbal of the vertical gyroscope. Movement of the roll and pitch gimbals registered roll and pitch axis sphere movement in relation to a miniature airplane symbol. A roll index, attached to the roll gimbal, indicated the roll displacement angle relative to a frame mounted roll scale. Pitch displacement angles were displayed on the sphere.  2, record 31, English, - pitch%20gimbal

Record 31,  Textual support,  French

Record number: 31, Textual support number: 1 CONT

Centrale de cap et de verticale pour avion. Une centrale est constituée d'un gyro-indicateur de verticale et d'un gyroscope directionnel garde-cap. La direction par rapport au nord du moment cinétique du gyroscope directionnel est repérée juste avant le départ de l'avion à l'aide d'un gyroscope de transfert. Un gyroscope de verticale asservit une plate-forme autour de deux axes parallèles aux axes de roulis et de tangage de l'avion. Cette plate-forme délivre les références de roulis et assiette longitudinale et supporte un gyroscope directionnel qui fonctionne en garde-cap. La plate-forme asservie est constituée d'un cadre de roulis extérieur et de deux cadres de tangage liés mécaniquement. À l'intérieur du premier cadre de tangage est placé le gyroscope de verticale, à l'intérieur du second le gyroscope directionnel [...]  1, record 31, French, - cadre%20de%20tangage

Record 31,  Textual support,  Spanish

Record 32,  Textual support,  English

Record number: 32, Textual support number: 1 CONT

The main AI [attitude indicator] used an electrically driven, two axis of freedom, vertical gyroscope assembly... Attitude information was displayed by a sphere which was mechanically driven by the pitch gimbal and directly attached to the roll gimbal of the vertical gyroscope. Movement of the roll and pitch gimbals registered roll and pitch axis sphere movement in relation to a miniature airplane symbol. A roll index, attached to the roll gimbal, indicated the roll displacement angle relative to a frame mounted roll scale. Pitch displacement angles were displayed on the sphere.  2, record 32, English, - roll%20gimbal

Record 32,  Textual support,  French

Record number: 32, Textual support number: 1 CONT

Centrale de cap et de verticale pour avion. Une centrale est constituée d'un gyro-indicateur de verticale et d'un gyroscope directionnel garde-cap. La direction par rapport au nord du moment cinétique du gyroscope directionnel est repérée juste avant le départ de l'avion à l'aide d'un gyroscope de transfert. Un gyroscope de verticale asservit une plate-forme autour de deux axes parallèles aux axes de roulis et de tangage de l'avion. Cette plate-forme délivre les références de roulis et assiette longitudinale et supporte un gyroscope directionnel qui fonctionne en garde-cap. La plate-forme asservie est constituée d'un cadre de roulis extérieur et de deux cadres de tangage liés mécaniquement. À l'intérieur du premier cadre de tangage est placé le gyroscope de verticale, à l'intérieur du second le gyroscope directionnel [...]  1, record 32, French, - cadre%20de%20roulis

Record 32,  Textual support,  Spanish

Record 33,  Textual support,  English

Record number: 33, Textual support number: 1 DEF

Dynamic measurement unit. Provides measurements of accelerations along three orthogonal axes and rotation rates around three orthogonal axes.  2, record 33, English, - dynamic%20measurement%20unit

Record number: 33, Textual support number: 1 CONT

The DMU-6 is an intelligent six axis measurement system designed for accurate acceleration and angle measurement in dynamic environments... Example applications include GPS navigation, dynamic positioning, and automotive testing. The DMU-VG outputs stabilized pitch and roll calculations in addition to the DMU-6 outputs, ideal for camera or platform stabilization.  3, record 33, English, - dynamic%20measurement%20unit

Record 33,  Textual support,  French

Record 33,  Textual support,  Spanish

Record 34,  Textual support,  English

Record number: 34, Textual support number: 1 CONT

During the first phase of rapid align, the liquid level signal controls the platform pitch erection. However... to avoid a large vertical error when the control of the platform pitch gimbal switches to the pitch pick-off in the second phase of rapid alignment, a phase reversal is required. The phase reversal is designed to keep all of the signal phasing correct while reversing the phase of the gyro pick-off signal. If the phase of the gyro pick-off were not reversed, the combined signals could null with a non-level gimbal and a non-vertical gyro spin axis. With the pick-off reversal, the same type of cancellation occurs but the gyro spin axis is vertical.  1, record 34, English, - gyro%20pick%2Doff%20signal

Record 34,  Textual support,  French

Record number: 34, Textual support number: 1 CONT

Durant la première phase de l'alignement rapide, le signal du niveau à liquide commande l'érection en tangage de la plate-forme. Cependant, il est nécessaire d'inverser la phase afin d'éviter un signal important d'erreur de verticale lorsque la commande du cardan de tangage de la plate-forme est donnée au détecteur de tangage durant la deuxième phase de l'alignement rapide. Cette inversion de phase est conçue pour garder la mise en phase correcte du signal lorsque la phase du signal détecteur du gyroscope est renversée. Si la phase du signal détecteur du gyroscope n'était pas inversée, les signaux composés pourraient devenir nuls avec un cardan qui ne serait pas correctement en érection et un axe de rotation qui ne serait pas à la verticale. En effectuant l'inversion du signal détecteur, le même genre d'annulation se produit mais l'axe de rotation du gyroscope est à la verticale.  1, record 34, French, - signal%20d%C3%A9tecteur%20du%20gyroscope

Record 34,  Textual support,  Spanish

Record 35,  Textual support,  English

Record number: 35, Textual support number: 1 CONT

During the second phase of alignment, the pitch component of the resolved LL [liquid level] is used to precess the gyro pitch axis in a direction to null the pitch component and thereby improve the pitch vertical alignment accuracy.  1, record 35, English, - pitch%20vertical%20alignment

Record 35,  Textual support,  French

Record number: 35, Textual support number: 1 CONT

Durant la deuxième phase de l'alignement, la composante de tangage du signal venant des niveaux à liquide est utilisée pour faire précessionner l'axe de tangage du gyroscope dans une direction telle qu'elle annule la composante de tangage et par conséquent, améliore la précision de l'alignement vertical de tangage.  1, record 35, French, - alignement%20vertical%20de%20tangage

Record 35,  Textual support,  Spanish

Record 36,  Textual support,  English

Record number: 36, Textual support number: 1 CONT

During heading align, the rotor of the resolver is positioned so that it transforms the N-S and E-W liquid level signals into pitch and roll components which are referenced to heading. The pitch component is amplified, demodulated and summed with amplified and demodulated feedback signals from the VG [vertical gyro] roll and pitch pickoffs and the pitch synchro. The combined signal is then modulated, amplified and converted to DC [direct current] to drive the platform pitch gimbal torque motor until the input signals are nulled.  2, record 36, English, - pitch%20pickoff

Record number: 36, Textual support number: 2 CONT

The AUTOFLUG FGC T is a cold-gas driven free displacement gyroscope concerning roll axis and yaw(pitch) axis. The FGC T consists of the following subassemblies : Gyroscope housing, gimbal bolt mechanism, gimbal system. Gyroscope drive consisting of : gas bottle and locking mechanism, roll pickoff, pitch pickoff and pickoff electronic.  3, record 36, English, - pitch%20pickoff

Record 36,  Textual support,  French

Record number: 36, Textual support number: 1 CONT

Les capteurs mesurant des angles autour d'axes proches de l'axe X du satellite sont généralement qualifiés de capteurs de roulis, les capteurs mesurant des angles autour d'axes proches de l'axe Y sont de même qualifiés de capteurs de tangage, et les capteurs mesurant des angles autour d'axes proches de l'axe Z sont qualifiés de capteurs de lacet. Ceci ne signifie pas que ces capteurs mesurent des angles de Cardan à partir d'un repère de référence inertiel, ils peuvent très bien mesurer par exemple un angle dièdre entre le plan (X, Z) et le plan (X, Soleil), on parlera dans ce cas d'un capteur de roulis Soleil.  2, record 36, French, - capteur%20de%20tangage

Record number: 36, Textual support number: 2 CONT

Durant l'alignement sur le cap, le rotor du résolver est mis en position de telle sorte qu'il transforme les signaux des niveaux à liquide N.-S. et E.-O. en composantes de tangage et de roulis en référence au cap. La composante de tangage est amplifiée, démodulée et composée avec des signaux de réaction amplifiés et démodulés venant des capteurs de roulis et de tangage du VG [gyroscope directionnel] et du synchro de tangage. Ce signal composé est alors modulé, amplifié et converti en courant continu pour entraîner le moteur couple du cardan de tangage de la plate-forme jusqu'à ce que les signaux d'entrée soient annulés.  3, record 36, French, - capteur%20de%20tangage

Record number: 36, Textual support number: 1 OBS

Quand le véhicule est connecté à un PC par un lien, l'interface permet d'agir directement sur les actionneurs (propulseur et gouvernes). Cette interface permet aussi de visualiser en temps réel, les données issues des capteurs : roulis, tangage, lacet, profondeur, vitesse de roulis et de tangage, ainsi que d'afficher les coordonnées fournies par le récepteur GPS.  4, record 36, French, - capteur%20de%20tangage

Record 36,  Textual support,  Spanish

Record 37,  Textual support,  English

Record number: 37, Textual support number: 1 CONT

During the first phase of rapid align, the liquid level signal controls the platform pitch erection. However... to avoid a large vertical error when the control of the platform pitch gimbal switches to the pitch pick-off in the second phase of rapid alignment, a phase reversal is required. The phase reversal is designed to keep all of the signal phasing correct while reversing the phase of the gyro pick-off signal. If the phase of the gyro pick-off were not reversed, the combined signals could null with a non-level gimbal and a non-vertical gyro spin axis. With the pick-off reversal, the same type of cancellation occurs but the gyro spin axis is vertical.  1, record 37, English, - pick%2Doff%20reversal

Record 37,  Textual support,  French

Record number: 37, Textual support number: 1 CONT

Durant le première phase de l'alignement rapide, le signal du niveau à liquide commande l'érection en tangage de la plate-forme. Cependant, il est nécessaire d'inverser la phase afin d'éviter un signal important d'erreur de verticale lorsque la commande du cardan de tangage de la plate-forme est donnée au détecteur de tangage durant la deuxième phase de l'alignement rapide. Cette inversion de phase est conçue pour garder la mise en phase correcte du signal lorsque la phase du signal détecteur du gyroscope est renversée. Si la phase du signal détecteur du gyroscope n'était pas inversée, les signaux composés pourraient devenir nuls avec un cardan qui ne serait pas correctement en érection et un axe de rotation qui ne serait pas à la verticale. En effectuant l'inversion du signal détecteur, le même genre d'annulation se produit mais l'axe de rotation du gyroscope est à la verticale.  1, record 37, French, - inversion%20du%20signal%20d%C3%A9tecteur

Record 37,  Textual support,  Spanish

Record 38,  Textual support,  English

Record number: 38, Textual support number: 1 OBS

vertical gyro : A two-degree-of-freedom gyro with provision for maintaining its spin axis vertical; output signals are produced by gimbal angular displacements which correspond to components of the angular displacements of the base about two orthogonal axes; used in aircraft to measure both bank angle and pitch attitude.  2, record 38, English, - two%20degree%20of%20freedom%20VG

Record 38,  Textual support,  French

Record number: 38, Textual support number: 1 OBS

Degrés de liberté. Le carter du gyroscope peut être lié au bâti qui le supporte de deux façons : la liaison est telle qu'elle autorise un mouvement de rotation autour d'un seul axe, le gyroscope est dit à un degré de liberté; la liaison est telle qu'elle autorise deux mouvements de rotation autour de deux axes concourants, le gyroscope est dit à deux degrés de liberté. Le carter peut exécuter une rotation quelconque autour du point de concours des deux axes.  2, record 38, French, - gyroscope%20de%20verticale%20%C3%A0%20deux%20degr%C3%A9s%20de%20libert%C3%A9

Record 38,  Textual support,  Spanish

Record 39,  Textual support,  English

Record number: 39, 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, record 39, English, - Station%26rsquo%3Bs%20flight%20attitude

Record number: 39, Textual support number: 1 OBS

Station’s flight attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 39, English, - Station%26rsquo%3Bs%20flight%20attitude

Record 39,  Textual support,  French

Record number: 39, 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, record 39, French, - attitude%20de%20la%20Station

Record number: 39, 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, record 39, French, - attitude%20de%20la%20Station

Record 39,  Textual support,  Spanish

Record 40,  Textual support,  English

Record number: 40, Textual support number: 1 CONT

The Ausroc 3(A3) launch vehicle has a liquid fuelled motor that burns JA-1 kerosene with liquid oxygen, and uses regenerative cooling. The motor produces 35 kN at sea level and has a burn time of 80 seconds. The motor is gimballed to facilitate pitch and yaw control. The wall of the combustion chamber, throat and expansion nozzle consists of 102 stainless steel tubes stacked side by side running parallel to the motor axis. The tubes will be brazed together and the assembly wrapped in a carbon fibre composite. The composite wrapping is used to relieve to tubes of the hoop stress generated by the combustion pressure(2 MPa), whilst the tubes contain the combustion heat(3500 K). The top end of the motor has a kerosene inlet manifolt, oxygen dome and injector block. The kerosene inlet manifold delivers kerosene to every second motor tube, where it travels down to the arse end of the motor. Here it enters the lower kerosene manifold which is a simple plenum ring. This allows the kerosene to flow into the other alternate tubes which deliver it back up to the inlet manifold. The inlet manifold then directs the kerosene to the injector block, which sprays it and the liquid oxygen into the combustion chamber.  2, record 40, English, - liquid%20fuelled%20motor

Record 40,  Textual support,  French

Record number: 40, Textual support number: 1 CONT

La fusée possède des moteurs à ergols liquides.  2, record 40, French, - moteur%20%C3%A0%20ergols%20liquides

Record 40,  Textual support,  Spanish

Record 41,  Textual support,  English

Record number: 41, Textual support number: 1 CONT

In the EO-1 experiment, the PPT will control the spacecraft pitch axis, temporarily replacing the corresponding momentum wheel in the primary attitude control system. The PPT will be used to counter environmental torque, generally firing at minimum energy levels.  2, record 41, English, - environmental%20torque

Record 41,  Textual support,  French

Record 41,  Textual support,  Spanish

Record 42,  Textual support,  English

Record number: 42, Textual support number: 1 CONT

The inclination of the orebody perpendicular to the strike will be its dip and the longest dimension of the orebody its axis. The plunge of the axis is measured in the vertical plane ABC but its pitch or rake can be measured in any other plane...  1, record 42, English, - axis

Record 42,  Textual support,  French

Record number: 42, Textual support number: 1 CONT

Axe du filon.  1, record 42, French, - axe

Record 42,  Textual support,  Spanish

Record 43,  Textual support,  English

Record number: 43, Textual support number: 1 CONT

The normal mode of control in the pitch axis is attitude hold, and in the yaw axis, the normal mode is attitude stabilization.  1, record 43, English, - attitude%20hold

Record 43,  Textual support,  French

Record 43,  Textual support,  Spanish

Record 44,  Textual support,  English

Record number: 44, Textual support number: 1 DEF

A circle the radius of which is equal to the distance from the gear axis to the pitch point.  2, record 44, English, - pitch%20circle

Record 44,  Textual support,  French

Record number: 44, Textual support number: 1 DEF

Section du cylindre primitif par un plan perpendiculaire à l'axe de la roue.  2, record 44, French, - cercle%20primitif

Record number: 44, Textual support number: 1 OBS

L'équivalent français est recommandé par l'Office de la langue française.  3, record 44, French, - cercle%20primitif

Record number: 44, Textual support number: 2 OBS

Cercle primitif [...] Ce terme peut être : ... de denture ou ... de fonctionnement.  2, record 44, French, - cercle%20primitif

Record 44,  Textual support,  Spanish

Record 45,  Textual support,  English

Record number: 45, Textual support number: 1 DEF

Degree of rotation of the rifling grooves. It can be constant or progressive, i. e. tightening in pitch as it nears the muzzle. The degree of twist can be defined by : the distance for the grooves to make a complete revolution, the number of calibres for one complete revolution, or the angle between the line of the groove and the axis of the bore. The sense of the twist, i. e. right-or left-hand as viewed from the breech, should also be specified, though very few firearms use a left-hand twist.  1, record 45, English, - twist%20of%20rifling

Record number: 45, Textual support number: 1 OBS

Term and definition officialized by the Small Arms Terminology Working Group.  2, record 45, English, - twist%20of%20rifling

Record 45,  Textual support,  French

Record number: 45, Textual support number: 1 DEF

Degré de rotation des rayures. Le pas peut être constant ou progressif, i.e. se resserrant en approchant de la bouche. Le pas de la rayure peut être déterminé par : la distance requise pour un tour complet des rayures, le nombre de calibres pour un tour complet ou l'angle entre la ligne de la rayure et l'axe de l'âme. Le sens du pas, soit à droite ou à gauche, vu de la culasse, devrait aussi être précisé, même si très peu d'armes à feu utilisent un pas à gauche.  1, record 45, French, - pas%20de%20la%20rayure

Record number: 45, Textual support number: 1 OBS

Terme et définition uniformisés par le Groupe de travail de terminologie des armes légères.  2, record 45, French, - pas%20de%20la%20rayure

Record 45,  Textual support,  Spanish

Record 46,  Textual support,  English

Record number: 46, Textual support number: 1 CONT

The electrical flying control system is based on two independent systems, the Elevator Aileron Computers(ELAC) and the Spoiler Elevator Computers(SEC). The first of these systems... is made up of a pair of computers which operate the ailerons for roll control, the elevator for pitch-axis control and the tailplane for automatic pitch axis trimming.  1, record 46, English, - elevator%20aileron%20computer

Record 46,  Textual support,  French

Record number: 46, Textual support number: 1 CONT

L'architecture des CDVE [commandes de vol électriques] comporte deux systèmes indépendants : l'ELAC (Elevator Aileron Computers = calculateurs de profondeur et d'ailerons) et le SEC (Spoiler and Elevator Computers = calculateurs de profondeur et des spoilers). Le système ELAC [...] est composé de deux calculateurs qui contrôlent les ailerons (fonction roulis), la gouverne de profondeur (tangage) et le stabilisateur horizontal arrière (fonction auto-trim).  1, record 46, French, - calculateur%20de%20profondeur%20et%20d%27ailerons

Record 46,  Textual support,  Spanish

Record 47,  Textual support,  English

Record number: 47, Textual support number: 1 CONT

The electrical flying control system is based on two independent systems, the Elevator Aileron Computers(ELAC) and the Spoiler Elevator Computers(SEC). The Spoiler Elevator Computer System... consists of a trio of computers, which will produce commands in the roll axis by operating the two outer spoiler panels on each wing; speed-braking in flight by operating the three inner spoiler panels; lift-dumping after landing by raising all ten spoiler panels; stand-by pitch axis control in support of the ELAC by operating the elevators and automatic trim, also as a stand-by to the ELAC, by adjusting tailplane incidence.  1, record 47, English, - spoiler%20elevator%20computer

Record 47,  Textual support,  French

Record number: 47, Textual support number: 1 CONT

L'architecture des CDVE [commandes de vol électriques] comporte deux systèmes indépendants : l'ELAC (Elevator Aileron Computers = calculateurs de profondeur et d'ailerons) et le SEC (Spoiler and Elevator Computers = calculateurs de profondeur et des spoilers). Le système SEC [...] comporte trois calculateurs qui contrôlent la fonction roulis des quatre spoilers extérieurs, la fonction aérofrein au sol par le déploiement des dix spoilers, la fonction tangage en secours de l'ELAC par action sur la gouverne de profondeur, et enfin la fonction auto-trim, également en secours de l'ELAC, par action sur le stabilisateur horizontal.  1, record 47, French, - calculateur%20de%20profondeur%20et%20des%20spoilers

Record 47,  Textual support,  Spanish

Record 48,  Textual support,  English

Record number: 48, Textual support number: 1 CONT

Several new functions have been integrated with the flight-management computer with the result that it has been renamed the Flight Management Guidance Computer(FMGC). The Flight Management Guidance Computer supplies command signals to the pitch and roll surfaces through the fly-by-wire computers and to the yaw axis through the flight-augmentation computers. Thrust management is vested in the FADEC engine controllers.  1, record 48, English, - flight%20management%20guidance%20computer

Record 48,  Textual support,  French

Record number: 48, Textual support number: 1 CONT

Le calculateur du FMS intègre quelques fonctions nouvelles, ce qui a amené à le rebaptiser FMGC (Flight Management Guidance Computer = calculateur de guidage et de gestion de vol). Le FMGC fournit les ordres de tangage et de roulis au travers des calculateurs des commandes de vol électriques, et contrôle le lacet par l'intermédiaire des calculateurs de stabilisation. La gestion de la poussée est confiée au système FADEC.  1, record 48, French, - calculateur%20de%20guidage%20et%20de%20gestion%20de%20vol

Record 48,  Textual support,  Spanish

Record 49,  Textual support,  English

Record 49,  Textual support,  French

Record number: 49, Textual support number: 1 OBS

Terme uniformisé par le CUTA opérations aériennes.  2, record 49, French, - calculateur%20de%20tangage

Record 49,  Textual support,  Spanish

Record 50,  Textual support,  English

Record number: 50, Textual support number: 1 DEF

A platform on which a person may be rotated in the pitch axis without any exertion to retain his position. Used in the study of the reaction of the circulatory system to a change of vector of the gravitational force, i. e. orthostatic tolerance.  1, record 50, English, - tilt%20table

Record 50,  Textual support,  French

Record number: 50, Textual support number: 1 DEF

Une plateforme sur laquelle une personne peut être basculée dans l'axe de tangage sans aucun effort de sa part pour garder sa position. Utilisée dans l'étude de la réaction du système circulatoire à l'égard d'une modification d'un vecteur de la force de gravité, par exemple dans l'étude de la tolérance à l'orthostatisme.  1, record 50, French, - table%20basculante

Record 50,  Textual support,  Spanish

Record 51,  Textual support,  English

Record number: 51, Textual support number: 1 DEF

A blade which is connected to its hub or central shaft through one or more joints about which the blade is free to move. Articulation generally refers to freedom about the blade pitch axis, but can include freedom in coning or freedom about other hub axes.  1, record 51, English, - articulated%20blade

Record 51,  Textual support,  French

Record number: 51, Textual support number: 1 CONT

(...) En Grande-Bretagne à St Albans, puis en Algérie à Grand-Vert, l'aérogénérateur Andreav Enfield d'une puissance minimale de 100 KW, cette machine avait la particularité d'avoir les pales articulées, réglées automatiquement de manière à maintenir constant le débit d'air dans la turbine.  1, record 51, French, - pale%20articul%C3%A9e

Record 51,  Textual support,  Spanish

Record 52,  Textual support,  English

Record 52,  Textual support,  French

Record number: 52, Textual support number: 1 OBS

(commande automatique)  1, record 52, French, - axes%20de%20tangage%20de%20roulis%20et%20de%20lacet

Record 52,  Textual support,  Spanish