TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

Originally, keyboard tablatures must have suggested a practical link to the keys of the instrument. Indeed, the anonymous tenth-century Bern organ treatise... describes the presence of pitch names, for the performer's visual reference, written directly on the keys of the organ. If letters of the alphabet could be used in this way, it is just as conceivable that numbers could have been used in a similar manner. Thus, the origin of "German" keyboard tablatures may be associated with the practice of lettered keys, and the origin of "Spanish" tablatures may, at least hypothetically, be associated with numbered keys.  2, record 1, English, - keyboard%20tablature

Record 1,  Textual support,  French

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

In the case of three-axis stabilization, also known as body stabilization, the stabilization is achieved by controlling the movement of the satellite along the three axes, i. e. yaw, pitch and roll, with respect to a reference... The system uses reaction wheels or momentum wheels to correct orbit perturbations.  2, record 2, English, - three%2Daxis%20stabilization

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 DEF

Stabilisation de l'orientation d'un engin spatial à l'aide d'un système d'asservissement permettant de maintenir trois axes liés à l'engin dans des directions déterminées.  1, record 2, French, - stabilisation%20sur%20trois%20axes

Record number: 2, Textual support number: 1 OBS

stabilisation sur trois axes; stabilisation trois axes : désignations et définition publiées au Journal officiel de la République française le 31 décembre 2005.  2, record 2, French, - stabilisation%20sur%20trois%20axes

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 DEF

Equipment that automatically stabilizes the attitude of an aircraft about its pitch, roll, and yaw axes and keeps it on a predetermined heading.  9, record 3, English, - automatic%20pilot

Record number: 3, Textual support number: 1 CONT

The gyropilot, commonly called an automatic pilot, consists basically of three devices, each of which detects disturbances of the aircraft in one plane and corrects for these disturbances by moving the appropriate control : the rudder control for azimuth and sudden change in heading(yaw) disturbances, aileron control for roll disturbance, and elevator control for pitch disturbance. In modern gyropilots rate detection forms the principal reference and displacement detection plays a secondary role.  6, record 3, English, - automatic%20pilot

Record number: 3, Textual support number: 1 OBS

automatic pilot; autopilot: terms officially approved by the International Civil Aviation Organization (ICAO).  10, record 3, English, - automatic%20pilot

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 DEF

Asservissement permettant d'automatiser le processus de correction de vol pour maintenir l'appareil sur une trajectoire sélectionnée.  5, record 3, French, - pilote%20automatique

Record number: 3, Textual support number: 1 OBS

La sélection peut s'effectuer au travers du Directeur de Vol (FD), ou directement à partir des indicateurs (Altimètre, cap, VOR/ILS).  5, record 3, French, - pilote%20automatique

Record number: 3, Textual support number: 2 OBS

système de pilotage automatique : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  6, record 3, French, - pilote%20automatique

Record number: 3, Textual support number: 3 OBS

pilote automatique; PA : terme et abréviation uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes; terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  7, record 3, French, - pilote%20automatique

Record number: 3, Textual support number: 4 OBS

pilote automatique : terme uniformisé par l'Organisation de l'aviation civile internationale (OACI).  8, record 3, French, - pilote%20automatique

Record number: 3, Textual support number: 1 PHR

PA numérique.  9, record 3, French, - pilote%20automatique

Record 3,  Textual support,  Spanish

Record number: 3, Textual support number: 1 OBS

piloto automático: término aceptado oficialmente por la Organización de Aviación Civil Internacional (OACI).  2, record 3, Spanish, - piloto%20autom%C3%A1tico

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 DEF

The quotient of the pitch at the reference surface, expressed in millimetres, divided by [pi].  2, record 4, English, - module

Record number: 4, Textual support number: 1 CONT

Module (inch) is the ratio of the pitch diameter in inches to the number of teeth. It is the reciprocal of the diametral pitch. Module (millimeter) is the ratio of the pitch diameter in millimeters to the number of teeth. It is converted to diametral pitch by the equation: P_d = 25.4/module (millimeters).  3, record 4, English, - module

Record number: 4, Textual support number: 1 OBS

Module may be in either inch or millimetre units. In inch units module is the reciprocal of the diametral pitch.  4, record 4, English, - module

Record number: 4, Textual support number: 2 OBS

module: term and definition standardized by ISO.  5, record 4, English, - module

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 DEF

Quotient du pas, mesuré sur la surface de référence, exprimé en millimètres, par le nombre [pi].  3, record 4, French, - module

Record number: 4, Textual support number: 1 OBS

module : terme et définition normalisés par l'ISO.  4, record 4, French, - module

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, 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 5, English, - pitch%20rate%20gyroscope

Record number: 5, 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 5, English, - pitch%20rate%20gyroscope

Record 5,  Textual support,  French

Record number: 5, 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 5, French, - gyrom%C3%A8tre%20de%20tangage

Record number: 5, Textual support number: 2 OBS

gyromètre de tangage : terme d'usage obligatoire au Bureau de la traduction du Canada.  4, record 5, French, - gyrom%C3%A8tre%20de%20tangage

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

For training purposes, turns are divided into three classes :(1) Gentle turns, involving angles of bank up to 15 degrees.(2) Medium turns...(3) Steep turns... In a gentle turn, the position of the nose in relation to the horizon, which is the visual reference for pitch attitude, will remain relatively the same as in straight and level flight.  2, record 6, English, - shallow%20turn

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 CONT

Aux fins de l'entraînement, on distingue trois sortes de virages : le virage à faible inclinaison, avec un angle d'inclinaison de 15 degrés au plus; le virage à inclinaison moyenne; [...] le virage serré [...] En virage à faible inclinaison, la position du capot par rapport à l'horizon sert de référence visuelle pour l'assiette longitudinale et elle doit demeurer relativement la même qu'en vol rectiligne en palier.  3, record 6, French, - virage%20%C3%A0%20faible%20inclinaison

Record number: 6, Textual support number: 1 OBS

virage à faible inclinaison : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  4, record 6, French, - virage%20%C3%A0%20faible%20inclinaison

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

Stabilisation and orientation [of a space vehicle] by inertial flywheels consists in accurately aligning the axes of three flywheels with the axes of reference(roll, pitch and yaw). When one of these flywheels is moved in yaw by an electric motor, its angular moment increases and the vehicle is subjected to a reactive couple. Inertial flywheels provide very fine control of orientation or stabilisation, because the couples set up may be very small.  1, record 7, English, - stabilisation%20by%20inertial%20flywheel

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 OBS

Les satellites ont besoin d'être dotés d'équipements permettant : - de repérer l'attitude du satellite par rapport à des repères extérieurs (terre, soleil); - de régler cette attitude en fonction des missions; - d'ajuster les paramètres de l'orbite. Ces fonctions sont assurées par le sous-système de stabilisation (mesure et contrôle d'attitude et d'orbite). Les roues à inertie sont un des dispositifs du sous-système de stabilisation et d'orientation.  2, record 7, French, - stabilisation%20par%20roue%20%C3%A0%20inertie

Record number: 7, Textual support number: 2 OBS

roue à inertie : Dispositif mécanique constitué par une masse équilibrée pouvant être mise en rotation dans un sens ou dans l'autre par un moteur électrique, permettant ainsi d'orienter finement un satellite.  2, record 7, French, - stabilisation%20par%20roue%20%C3%A0%20inertie

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, 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 8, English, - spherical%20orienter

Record 8,  Textual support,  French

Record number: 8, 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 8, French, - syst%C3%A8me%20d%27orientation%20gyroscopique

Record number: 8, 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 8, French, - syst%C3%A8me%20d%27orientation%20gyroscopique

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, 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 9, English, - roll%20axis

Record number: 9, 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 9, English, - roll%20axis

Record number: 9, 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 9, English, - roll%20axis

Record number: 9, 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 9, English, - roll%20axis

Record 9,  Textual support,  French

Record number: 9, 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 9, French, - axe%20de%20roulis

Record number: 9, 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 9, French, - axe%20de%20roulis

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, 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 10, English, - pitch%20axis

Record number: 10, 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 10, English, - pitch%20axis

Record number: 10, 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 10, English, - pitch%20axis

Record number: 10, 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 10, English, - pitch%20axis

Record 10,  Textual support,  French

Record number: 10, 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 10, French, - axe%20de%20tangage

Record number: 10, 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 10, French, - axe%20de%20tangage

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 DEF

The quotient of the number [pi] divided by the pitch, expressed in inches, or the quotient of the number of teeth divided by the reference diameter, expressed in inches.  1, record 11, English, - diametral%20pitch

Record number: 11, Textual support number: 1 OBS

diametral pitch: term and definition standardized by ISO.  2, record 11, English, - diametral%20pitch

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 DEF

Quotient du nombre [pi] par le pas, exprimé en inches, ou quotient du nombre de dents par le diamètre de référence exprimé en inches.  3, record 11, French, - diametral%20pitch

Record number: 11, Textual support number: 1 OBS

diametral pitch : terme et définition normalisés par l'ISO.  4, record 11, French, - diametral%20pitch

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 DEF

The quotient of the transverse pitch, expressed in millimetres, divided by the number [pi](or the quotient of the reference diameter expressed in millimetres, divided by the number of teeth).  2, record 12, English, - transverse%20module

Record number: 12, Textual support number: 1 OBS

transverse module: term and definition standardized by ISO.  3, record 12, English, - transverse%20module

Record 12,  Textual support,  French

Record number: 12, Textual support number: 1 DEF

Quotient du pas apparent, exprimé en millimètres, par le nombre [pi] (ou quotient du diamètre de référence, exprimé en millimètres, par le nombre de dents).  2, record 12, French, - module%20apparent

Record number: 12, Textual support number: 1 OBS

module apparent : terme et définition normalisés par l'ISO.  3, record 12, French, - module%20apparent

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 DEF

The rotation of a vehicle about its vertical (Z) axis, i.e. movement in azimuth.  2, record 13, English, - yaw

Record number: 13, 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 13, English, - yaw

Record number: 13, 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 13, English, - yaw

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 DEF

Mouvement d'un corps autour d'un axe perpendiculaire aux axes de roulis et de tangage.  2, record 13, French, - lacet

Record number: 13, 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 13, French, - lacet

Record number: 13, 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 13, French, - lacet

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 DEF

Incline of a roof expressed as a ratio of vertical rise to horizontal run. For example, a roof that rises at the rate of 4 in. for each 12 in. of run is designated as having a 4 in. 12 slope.  8, record 14, English, - pitch

Record number: 14, Textual support number: 1 CONT

The slope of a roof is generally referred to as the pitch and is expressed as the ratio of the rise of the roof to the horizontal span.  9, record 14, English, - pitch

Record number: 14, Textual support number: 1 OBS

Slope indicates the incline of a roof as a ratio of vertical rise to horizontal run .... Slope and pitch are often incorrectly used synonymously when referring to the incline of a sloped roof. Pitch indicates the incline of a roof as a ratio of the vertical rise to twice the horizontal run.  10, record 14, English, - pitch

Record number: 14, Textual support number: 2 OBS

The distinction between "slope" and "pitch" traced in "Construction : Principles, Materials, and Methods, "by Harold B. Olin, et al(source OLICO) can also be found in "Construction Glossary : an encyclopedic reference and manual, "by J. Stewart Stein(source SCONS, p 275), but nowhere else.  11, record 14, English, - pitch

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 DEF

Inclinaison d'un versant. (Elle s'exprime soit en degrés mesurés sur l'angle que forme l'horizontale avec la couverture, soit en hauteur mesurée sur la perpendiculaire.)  3, record 14, French, - pente

Record number: 14, Textual support number: 1 CONT

(...) la pente d'un toit, c'est le rapport entre son élévation et sa course. Prends, par exemple, un toit ayant une élévation de 2 000 mm et une course de 6 000 mm. Le rapport élévation : course est donc de 2 000 : 6 000 mais, pour uniformiser, on parle d'une pente de 1 : 3.  4, record 14, French, - pente

Record number: 14, Textual support number: 1 OBS

Noter que pour certains auteurs la pente ne doit pas être confondue avec l'inclinaison; la pente exprime un rapport entre l'élévation et la course du toit, alors que l'inclinaison est une mesure de l'angle formé avec le plan horizontal, exprimée en degrés.  8, record 14, French, - pente

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 CONT

An azimuth gimbal assembly contains a DG [directional gyro] stabilized in pitch and roll for establishing A/C [aircraft] heading reference, two liquid levels oriented N-S and E-W for platform erection error sensing, and azimuth gimbal servo torquer, two azimuth synchro control transmitters and two mercury switches oriented N-S and E-W for erection cut-off when accelerations exceed. 23 G.  1, record 15, English, - platform%20erection%20error

Record 15,  Textual support,  French

Record number: 15, Textual support number: 1 CONT

L'ensemble azimutal monté sur cardan [...] comprend un [gyroscope] directionnel stabilisé sur les axes de roulis et de tangage et servant à établir le cap de l'aéronef, deux niveaux à liquide dont l'un est orienté en direction N.-S. et l'autre, en direction E.-O. et servant à détecter l'erreur d'érection de la plate-forme, un servomoteur couple [...] du cardan azimutal, deux transmetteurs de synchro détection azimutale [...] et deux interrupteurs à mercure [...] qui coupent le circuit d'érection lorsque l'accélération dépasse .23g.  1, record 15, French, - erreur%20d%27%C3%A9rection%20de%20la%20plate%2Dforme

Record number: 15, Textual support number: 1 OBS

Pluriel : des plateformes, des plates-formes.  2, record 15, French, - erreur%20d%27%C3%A9rection%20de%20la%20plate%2Dforme

Record number: 15, Textual support number: 2 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).  3, record 15, French, - erreur%20d%27%C3%A9rection%20de%20la%20plate%2Dforme

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 DEF

Half the algebraic difference between the reference diameter and the pitch diameter.  1, record 16, English, - profile%20shift

Record number: 16, Textual support number: 1 OBS

It is equal to the specified centre distance, minus half of the sum of the reference diameter of the worm and the pitch diameter of the wheel.  1, record 16, English, - profile%20shift

Record number: 16, Textual support number: 2 OBS

Terminology of worm gear geometry.  2, record 16, English, - profile%20shift

Record number: 16, Textual support number: 3 OBS

profile shift: term and definition standardized by ISO.  2, record 16, English, - profile%20shift

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 DEF

Demi-différence algébrique entre le diamètre de référence et le diamètre de fonctionnement de la roue.  1, record 16, French, - d%C3%A9port

Record number: 16, Textual support number: 1 OBS

[Le déport] est la différence, positive ou négative, entre l'entraxe de l'engrenage et la demi-somme du diamètre de référence de la vis et du diamètre de fonctionnement de la roue.  1, record 16, French, - d%C3%A9port

Record number: 16, Textual support number: 2 OBS

Terminologie de la géométrie des engrenages à vis.  2, record 16, French, - d%C3%A9port

Record number: 16, Textual support number: 3 OBS

déport : terme et définition normalisés par l'ISO.  2, record 16, French, - d%C3%A9port

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 CONT

To recover from the microburst, the crew apply maximum power and pitch up toward an angle that can attain 15 degrees. The inertial acceleration(acceleration in reference to the ground, as opposed to acceleration within the airmass) experienced by the pilots, combined with the unstable attitude of the aircraft may cause a dangerous illusion. The pilots may believe that the aircraft has reached a very high excess energy and thus, try to pitch down or reduce the engine power. In reality, the aircraft performance is still low as it penetrates the energy-reducing downdraft and tailwind components of the microburst.  2, record 17, English, - inertial%20acceleration

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 CONT

Rossby (nombre de) : Quantité sans dimension, utile dans l'étude du mouvement des atmosphères planétaires et égale au rapport de l'accélération inertielle (force d'inertie) à l'accélération de Coriolis due à la rotation de la planète.  2, record 17, French, - acc%C3%A9l%C3%A9ration%20inertielle

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, Textual support number: 1 CONT

An azimuth gimbal assembly contains a DG [directional gyro] stabilized in pitch and roll for establishing A/C [aircraft] heading reference, two liquid levels oriented N-S and E-W for platform erection error sensing, an azimuth gimbal servo torquer, two azimuth synchro control transmitters and two mercury switches oriented N-S and E-W for erection cut-off when accelerations exceed. 23 G.  1, record 18, English, - azimuth%20gimbal%20assembly

Record 18,  Textual support,  French

Record number: 18, Textual support number: 1 CONT

L'ensemble azimutal monté sur cardan [...] comprend un directionnel stabilisé sur les axes de roulis et de tangage et servant à établir le cap de l'aéronef, deux niveaux à liquide dont l'un est orienté en direction N.-S. et l'autre, en direction E.-O. et servant à détecter l'erreur d'érection de la plate-forme, un servomoteur couple [...] du cardan azimutal, deux transmetteurs de synchrodétection azimutale [...] et deux rupteurs à mercure [...] orientés l'un vers le N.-S. et l'autre vers E.-O., qui coupent le circuit d'érection lorsque l'accélération dépasse .23g.  1, record 18, French, - ensemble%20azimutal%20mont%C3%A9%20sur%20cardan

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, 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 19, English, - inertial%20reference

Record 19,  Textual support,  French

Record number: 19, 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 19, French, - r%C3%A9f%C3%A9rence%20inertielle

Record number: 19, 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 19, French, - r%C3%A9f%C3%A9rence%20inertielle

Record 19,  Textual support,  Spanish

Record 20,  Textual support,  English

Record number: 20, Textual support number: 1 CONT

The attitude indicator (also called the artificial horizon or the gyro horizon) provides the pilot with an artificial horizon as a means of reference when the natural horizon cannot be seen because of cloud, fog, rain or other obstructions to visibility... The natural horizon is represented by a horizon bar on the face of the instrument.  4, record 20, English, - natural%20horizon

Record number: 20, Textual support number: 2 CONT

The attitude indicator relies on the principle of gyroscopic rigidity in space--the rapidly-spinning rotor disk resists any attempt to disturb its orientation. Thus, the gyro provides a stable horizontal reference against which the pitch and roll attitudes of the aircraft can be measured. The "artificial horizon bar" on the face of the attitude indicator is mechanically coupled to the gyro inside, so it remains parallel to the natural horizon. The instrument's little "symbolic airplane" is fixed to the instrument case, however, so it follows the roll and pitch movements of the real airplane. Consequently, the relationship of the horizon bar to the symbolic airplane is the same as the relationship between the natural horizon and the real airplane.  5, record 20, English, - natural%20horizon

Record number: 20, Textual support number: 3 CONT

The attitude indicator and heading indicator are based on a gyro’s rigidity in space. Because a gyro resists being tipped over, it can provide a stable reference to the real horizon or to a specific direction.  2, record 20, English, - natural%20horizon

Record 20,  Textual support,  French

Record number: 20, Textual support number: 1 CONT

Horizon artificiel. Cet instrument gyroscopique indique au pilote la position des ailes et du nez de l'avion par rapport à l'horizon terrestre lorsque l'horizon naturel n'est pas visible en raison des nuages, du brouillard, de la pluie.  2, record 20, French, - horizon%20naturel

Record number: 20, Textual support number: 2 CONT

En cas de perte des références extérieures, (rentrer dans un nuage, forte dégradation de la visibilité par brume ou pluie...), le pilote ne disposera plus que d'une vision réduite de son environnement par l'intermédiaire de l'horizon artificiel. Cet instrument sera - au même titre que l'horizon naturel en pilotage à vue - sa référence principale.  4, record 20, French, - horizon%20naturel

Record number: 20, Textual support number: 3 CONT

L'horizon artificiel dont se servent les pilotes d'avion est produit par un gyroscope en mouvement. Cet instrument est extrêmement important pour les pilotes puisqu'il leur indique la position de l'avion par rapport à l'horizon vrai.  3, record 20, French, - horizon%20naturel

Record number: 20, Textual support number: 1 OBS

Les termes «horizon terrestre» et «horizon naturel» ne sont pas de parfaits synonymes mais, en contexte de pilotage avion, on peut penser que les deux termes se confondent.  5, record 20, French, - horizon%20naturel

Record 20,  Textual support,  Spanish

Record 21,  Textual support,  English

Record number: 21, 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). When one of these flywheels is moved in yaw by an electric motor, its angular moment increases and the vehicle is subjected to a reactive couple. Inertial flywheels provide very fine control of orientation or stabilisation, because the couples set up may be very small.  1, record 21, English, - inertial%20flywheel

Record 21,  Textual support,  French

Record number: 21, Textual support number: 1 DEF

Dispositif mécanique constitué par une masse équilibrée pouvant être mise en rotation dans un sens ou dans l'autre par un moteur électrique, permettant ainsi d'orienter finement un satellite.  1, record 21, French, - roue%20%C3%A0%20inertie

Record number: 21, Textual support number: 1 CONT

Les satellites ont besoin d'être dotés d'équipements permettant : - de repérer l'attitude du satellite par rapport à des repères extérieurs (terre, soleil); - de régler cette attitude en fonction des missions; - d'ajuster les paramètres de l'orbite. Ces fonctions sont assurées par le sous-système de stabilisation (mesure et contrôle d'attitude et d'orbite). Les roues à inertie sont un des dispositifs du sous-système de stabilisation et d'orientation. Il existe deux grands types de roue à inertie : - les roues à paliers classiques (roulements à billes); - les roues à paliers magnétiques (suppression des frottements mécaniques permettant une minimisation des vibrations). Les roues à paliers magnétiques équipent les satellites «Spot».  1, record 21, French, - roue%20%C3%A0%20inertie

Record number: 21, Textual support number: 2 CONT

Après 3 ans en orbite surchauffe du volant à inertie permettant la stabilisation du satellite.  3, record 21, French, - roue%20%C3%A0%20inertie

Record 21,  Textual support,  Spanish

Record 22,  Textual support,  English

Record number: 22, Textual support number: 1 CONT

The basic attitude sensor was the three-gyro inertial reference package. It contained two air-tight integrating gyro units to sense pitch and yaw, and one miniature integrating gyro unit to sense roll. The pitch and roll gyros were torqued by signals obtained by two Barnes mod IIA infrared horizon sensors. Gyrocompassing oriented the vehicle to an orbit plane yaw reference by detecting a component of the programmed pitch rate through the roll horizon sensor. The geocentric pitch rate(typically 4 deg/min, for a low-altitude orbit) was programmed as a constant torque to the pitch gyro. This pitch component, if a yaw error was present, would be sensed differentially when compared with the roll components of the two horizon-sensor heads. The differential would be seen as a function of yaw error.  2, record 22, English, - roll%20component

Record number: 22, Textual support number: 2 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.  1, record 22, English, - roll%20component

Record 22,  Textual support,  French

Record number: 22, Textual support number: 1 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.  2, record 22, French, - composante%20en%20roulis

Record number: 22, Textual support number: 2 CONT

Il s'agit de la rotation galiléenne mais [...] la rotation à annuler quand on souhaite obtenir un pointage Terre parfait est la rotation relative au repère orbital de composantes en roulis, tangage et lacet.  1, record 22, French, - composante%20en%20roulis

Record 22,  Textual support,  Spanish

Record 23,  Textual support,  English

Record number: 23, Textual support number: 1 CONT

The basic attitude sensor was the three-gyro inertial reference package. It contained two air-tight integrating gyro units to sense pitch and yaw, and one miniature integrating gyro unit to sense roll. The pitch and roll gyros were torqued by signals obtained by two Barnes mod IIA infrared horizon sensors. Gyrocompassing oriented the vehicle to an orbit plane yaw reference by detecting a component of the programmed pitch rate through the roll horizon sensor. The geocentric pitch rate(typically 4 deg/min, for a low-altitude orbit) was programmed as a constant torque to the pitch gyro. This pitch component, if a yaw error was present, would be sensed differentially when compared with the roll components of the two horizon-sensor heads. The differential would be seen as a function of yaw error.  2, record 23, English, - pitch%20component

Record number: 23, Textual support number: 2 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.  3, record 23, English, - pitch%20component

Record 23,  Textual support,  French

Record number: 23, Textual support number: 1 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.  2, record 23, French, - composante%20en%20tangage

Record number: 23, Textual support number: 2 CONT

[...] il s'agit de la rotation galiléenne mais [...] la rotation à annuler quand on souhaite obtenir un pointage Terre parfait est la rotation relative au repère orbital de composantes en roulis, tangage et lacet.  1, record 23, French, - composante%20en%20tangage

Record 23,  Textual support,  Spanish

Record 24,  Textual support,  English

Record number: 24, Textual support number: 1 CONT

An azimuth gimbal assembly contains a DG [directional gyro] stabilized in pitch and roll for establishing A/C [aircraft] heading reference, two liquid levels oriented N-S and E-W for platform erection error sensing, an azimuth gimbal servo torquer, two azimuth synchro control transmitters and two mercury switches oriented N-S and E-W for erection cut-off when accelerations exceed. 23 G.  1, record 24, English, - azimuth%20synchro%20control%20transmitter

Record 24,  Textual support,  French

Record number: 24, Textual support number: 1 CONT

L'ensemble azimutal monté sur cardan [...] comprend un directionnel stabilisé sur les axes de roulis et de tangage et servant à établir le cap de l'aéronef, deux niveaux à liquide dont l'un est orienté en direction N.-S. et l'autre, en direction E.-O. et servant à détecter l'erreur d'érection de la plate-forme, un servomoteur couple [...] du cardan azimutal, deux transmetteurs de synchrodétection azimutale [...] et deux rupteurs à mercure [...] orientés l'un vers le N.-S. et l'autre vers E.-O., qui coupent le circuit d'érection lorsque l'accélération dépasse .23g.  1, record 24, French, - transmetteur%20de%20synchrod%C3%A9tection%20azimutale

Record 24,  Textual support,  Spanish

Record 25,  Textual support,  English

Record number: 25, Textual support number: 1 CONT

The GHARS performs the functions of an all attitude flight reference system, providing an accurate, reliable, inertially stabilized heading and vertical reference for true and grid navigation, for aircraft stabilization and weapons control system, continuous pitch, roll and heading data for attitude and heading instruments in both fixed and rotary winged aircraft.  1, record 25, English, - gyroscopic%20heading%20and%20attitude%20reference%20system

Record 25,  Textual support,  French

Record number: 25, Textual support number: 1 CONT

Le Fokker 27 [...] Comme moyen secondaire de contrôle d'attitude, une centrale gyroscopique de cap et de verticale (SFIM type 550-2) est utilisée. Le bloc gyroscopique de la centrale est placé sur les têtes optiques des scanners. La vanne de flux est implantée dans une zone amagnétique (aile).  3, record 25, French, - centrale%20gyroscopique%20de%20cap%20et%20de%20verticale

Record 25,  Textual support,  Spanish

Record 26,  Textual support,  English

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

Record number: 26, Textual support number: 1 OBS

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

Record 26,  Textual support,  French

Record number: 26, 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 26, French, - attitude%20de%20la%20Station

Record number: 26, 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 26, French, - attitude%20de%20la%20Station

Record 26,  Textual support,  Spanish

Record 27,  Textual support,  English

Record number: 27, Textual support number: 1 CONT

The gyropilot, commonly called an automatic pilot(q. v.), consists basically of three devices, each of which detects disturbances for the aircraft in one plane and corrects for these disturbances by moving the appropriate control : the rudder control for azimuth and sudden change in heading(yaw) disturbances, aileron control for roll disturbance, and elevator control for pitch disturbance. In modern gyropilots rate detection forms the principal reference and displacements detection plays a secondary role. In such designs yaw disturbance is detected by a rate gyroscope and the change in heading is detected by the associated gyrocompass.  1, record 27, English, - yaw%20disturbance

Record number: 27, Textual support number: 1 OBS

yaw: The rotational or oscillatory movement of a ship, aircraft, rocket, or the like about a vertical axis.  3, record 27, English, - yaw%20disturbance

Record 27,  Textual support,  French

Record number: 27, Textual support number: 1 CONT

La stéréoscopie est obtenue à partir de visées acquises selon des dépointages latéraux différents [...]. De ce fait les deux images du couple sont acquises au cours d'orbites différentes. [...] La stéréoscopie latérale est affectée par les perturbations d'attitude en roulis. [...] La stéréoscopie longitudinale est affectée par les perturbations d'attitude en tangage et lacet.  1, record 27, French, - perturbation%20d%27attitude%20en%20lacet

Record 27,  Textual support,  Spanish

Record 28,  Textual support,  English

Record number: 28, Textual support number: 1 DEF

Vertical height from the GRP [ground reference plane] to a "Z" plane containing the lower edge of the blade cutting edge when this edge is in an "X" plane. If blace pitch is adjustable, blade pitch angle shall be adjusted for maximum lift above the ground.  1, record 28, English, - lift%20above%20ground

Record number: 28, Textual support number: 1 OBS

Graders terminology.  2, record 28, English, - lift%20above%20ground

Record number: 28, Textual support number: 2 OBS

Term and definition standardized by ISO.  2, record 28, English, - lift%20above%20ground

Record 28,  Textual support,  French

Record number: 28, Textual support number: 1 DEF

Hauteur verticale à partir du PRS [plan de référence au sol] jusqu'à un plan à la cote "Z" contenant l'arête inférieure du bord de coupe de la lame, quand ce bord se trouve dans un plan "X". Si l'angle d'attaque de la lame est réglable, il doit être réglé pour une levée maximale au-dessus du sol.  1, record 28, French, - lev%C3%A9e%20au%2Ddessus%20du%20sol

Record number: 28, Textual support number: 1 OBS

Terminologie des niveleuses.  2, record 28, French, - lev%C3%A9e%20au%2Ddessus%20du%20sol

Record number: 28, Textual support number: 2 OBS

Terme et définition normalisés par l'ISO.  2, record 28, French, - lev%C3%A9e%20au%2Ddessus%20du%20sol

Record 28,  Textual support,  Spanish

Record 29,  Textual support,  English

Record number: 29, Textual support number: 1 DEF

Distance on "X" coordinate between an "X" plane through the centreline of the front wheels and an "X" plane through the front edge of the cutting edge with the edge on the ground reference plane(GRP). If blade pitch is adjustable, blade pitch angle to be at the mid-point of the adjustment.  1, record 29, English, - blade%20base

Record number: 29, Textual support number: 1 OBS

Graders terminology.  2, record 29, English, - blade%20base

Record number: 29, Textual support number: 2 OBS

Term and definition standardized by ISO.  2, record 29, English, - blade%20base

Record 29,  Textual support,  French

Record number: 29, Textual support number: 1 DEF

Distance, sur l'axe de coordonnée "X", entre un plan vertical passant par l'axe des roues avant et un plan vertical passant par l'arête frontale du bord de coupe, ce bord se trouvant sur le PRS [plan de référence au sol]. Si l'angle d'attaque de la lame est réglable, il doit se trouver en position centrale de réglage.  1, record 29, French, - base%20de%20la%20lame

Record number: 29, Textual support number: 1 OBS

Terminologie des niveleuses.  2, record 29, French, - base%20de%20la%20lame

Record number: 29, Textual support number: 2 OBS

Terme et définition normalisés par l'ISO.  2, record 29, French, - base%20de%20la%20lame

Record 29,  Textual support,  Spanish

Record 30,  Textual support,  English

Record number: 30, Textual support number: 1 DEF

The quotient of the difference, expressed in millimetres, between centre distance and reference centre distance by the module, or the product of this difference, expressed in inches, by the diametral pitch.  1, record 30, English, - centre%20distance%20modification%20coefficient

Record number: 30, Textual support number: 1 OBS

[Centre distance modification coefficient] is a translation of the French term [coefficient de modification d’entr’axe] for which there is no corresponding special term in English.  1, record 30, English, - centre%20distance%20modification%20coefficient

Record number: 30, Textual support number: 2 OBS

Term and definition standardized by ISO.  2, record 30, English, - centre%20distance%20modification%20coefficient

Record 30,  Textual support,  French

Record number: 30, Textual support number: 1 DEF

Quotient de la différence, exprimée en millimètres, entre l'entr'axe et l'entr'axe de référence par le module, ou produit de cette différence, exprimée en inches, par le diametral pitch.  1, record 30, French, - coefficient%20de%20modification%20d%27entr%27axe

Record number: 30, Textual support number: 1 OBS

Terme et définition normalisés par l'ISO.  2, record 30, French, - coefficient%20de%20modification%20d%27entr%27axe

Record 30,  Textual support,  Spanish

Record 31,  Textual support,  English

Record number: 31, Textual support number: 1 DEF

The quotient of the number [pi] to the transverse pitch expressed in inches(or the quotient of the number of teeth to the reference diameter expressed in inches).  1, record 31, English, - transverse%20diametral%20pitch

Record number: 31, Textual support number: 1 OBS

Term and definition standardized by ISO.  2, record 31, English, - transverse%20diametral%20pitch

Record 31,  Textual support,  French

Record number: 31, Textual support number: 1 DEF

Quotient du nombre [pi] par le pas apparent, exprimé en inches (ou quotient du nombre de dents par le diamètre primitif, exprimé en inches).  1, record 31, French, - diametral%20pitch%20apparent

Record number: 31, Textual support number: 1 OBS

Terme et définition normalisés par l'ISO.  2, record 31, French, - diametral%20pitch%20apparent

Record 31,  Textual support,  Spanish

Record 32,  Textual support,  English

Record number: 32, Textual support number: 1 CONT

While the Autopilot system is disengaged, the heading, roll and pitch signals from gyro data systems are used to synchronize the reference heading and attitude circuits, so as to prevent jerky engagement.  1, record 32, English, - jerky%20engagement

Record 32,  Textual support,  French

Record number: 32, Textual support number: 1 CONT

Tant que le pilote automatique n'est pas engagé, les signaux de roulis, de cap et de tangage provenant des systèmes de référence gyroscopiques sont utilisés pour synchroniser les dispositifs de référence d'assiette et de cap. Ceci a pour but d'empêcher des réactions brusques à l'engagement.  1, record 32, French, - r%C3%A9actions%20brusques%20%C3%A0%20l%27engagement

Record 32,  Textual support,  Spanish

Record 33,  Textual support,  English

Record number: 33, Textual support number: 1 CONT

After engagement(of the autopilot the) reference signals(heading, roll and pitch) are added to the pilot's manual control signals in order to provide command signals to the amplifier servo modules.  1, record 33, English, - amplifier%20servo%20module

Record 33,  Textual support,  French

Record number: 33, Textual support number: 1 CONT

Quand le pilote automatique est engagé (les) signaux (de roulis, de cap et de tangage) s'ajoutent aux signaux amplifiés de commande manuelle d'évolution, afin de fournir des signaux de commande aux servo-amplificateurs.  1, record 33, French, - module%20servo%2Damplificateur

Record 33,  Textual support,  Spanish

Record 34,  Textual support,  English

Record 34,  Textual support,  French

Record number: 34, Textual support number: 1 OBS

terme d'usage obligatoire au Bureau des Traductions.  2, record 34, French, - r%C3%A9f%C3%A9rence%20en%20tangage

Record 34,  Textual support,  Spanish

Record 35,  Textual support,  English

Record 35,  Textual support,  French

Record number: 35, Textual support number: 1 OBS

terme d'usage obligatoire au Bureau des Traductions.  2, record 35, French, - point%20de%20r%C3%A9f%C3%A9rence%20en%20tangage

Record 35,  Textual support,  Spanish

Record 36,  Textual support,  French

Record 36,  Textual support,  Spanish