TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

For example, if the aircraft is descending at 1, 000 fpm, start the level off 100 feet above the level off altitude. If the pitch attitude change is started late, there is a tendency to overshoot the desired altitude unless the pitch change is made with a rapid movement.  2, record 1, English, - level%2Doff%20altitude

Record 1,  Textual support,  French

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

[The] attitude control subsystem(ACS) has yaw, roll, and pitch sensors that enable the attitude control processor(ACP) to maintain altitude accurately.  2, record 2, English, - attitude%20control%20processor

Record 2,  Textual support,  French

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

Over a slightly longer interval, pitch attitude will integrate into vertical speed and deviation from an assigned attitude, and roll attitude will integrate into heading; thus, display of aircraft vertical speed, altitude and heading should be positioned around the attitude display.  2, record 3, English, - attitude%20display

Record number: 3, Textual support number: 1 OBS

attitude display: term officially approved by the Aeronautical Terminology Standardization Committee (the ATSC) - Helicopters.  3, record 3, English, - attitude%20display

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

affichage d'assiette : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Hélicoptères.  2, record 3, French, - affichage%20d%27assiette

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

The command bars move up for a climb or down for descent, and roll left or right to provide lateral guidance. They display the computed angle of bank for standard-rate turns to enable the pilot to reach and fly a selected heading or track. The bars also show pitch commands that allow the pilot to capture and fly an ILS [instrument landing system] glide slope, a preselected pitch attitude, or maintain a selected barometric altitude.  2, record 4, English, - pitch%20command

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 OBS

directive en tangage : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA)- Opérations aériennes.  2, record 4, French, - directive%20en%20tangage

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 DEF

A movable horizontal airfoil, usually attached to the horizontal stabilizer on the tail, that is used to control pitch[;] it usually changes the attitude of the nose, making it move up and down.  2, record 5, English, - elevator

Record number: 5, Textual support number: 1 OBS

control surface: Any external moveable part of an aircraft designed to help it change orientation or speed, not including the propeller. The most commonly used control surfaces are ailerons, elevator, rudder, flaps, and spoilers.  3, record 5, English, - elevator

Record number: 5, Textual support number: 2 OBS

elevator: term standardized by ISO and NATO.  4, record 5, English, - elevator

Record number: 5, Textual support number: 1 PHR

Up-elevator, horizontal elevator.  5, record 5, English, - elevator

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 DEF

Volet mobile situé sur le bord de fuite du plan horizontal de l'empennage.  4, record 5, French, - gouverne%20de%20profondeur

Record number: 5, Textual support number: 1 CONT

gouverne : Chacun des organes utilisés pour obtenir la rotation d'un aéronef autour de ses trois axes : tangage (gouverne de profondeur), roulis (gouverne latérale), lacet (gouverne de direction) et constitués, généralement, par des plans mobiles actionnés par le pilote au moyen du palonnier (lacet) et du manche à balai (tangage et roulis).  5, record 5, French, - gouverne%20de%20profondeur

Record number: 5, Textual support number: 1 OBS

gouverne de profondeur : terme normalisé par l'ISO et l'OTAN.  6, record 5, French, - gouverne%20de%20profondeur

Record number: 5, Textual support number: 2 OBS

gouverne de profondeur; profondeur : termes uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  6, record 5, French, - gouverne%20de%20profondeur

Record 5,  Textual support,  Spanish

Record number: 5, Textual support number: 1 DEF

Superficie aerodinámica móvil situada en posición horizontal y en el empenaje de cola que permite realizar el control de profundidad.  3, record 5, Spanish, - tim%C3%B3n%20de%20altura

Record 6,  Textual support,  English

Record number: 6, 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 6, English, - automatic%20pilot

Record number: 6, 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 6, English, - automatic%20pilot

Record number: 6, Textual support number: 1 OBS

automatic pilot; autopilot: terms officially approved by the International Civil Aviation Organization (ICAO).  10, record 6, English, - automatic%20pilot

Record 6,  Textual support,  French

Record number: 6, 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 6, French, - pilote%20automatique

Record number: 6, 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 6, French, - pilote%20automatique

Record number: 6, 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 6, French, - pilote%20automatique

Record number: 6, 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 6, French, - pilote%20automatique

Record number: 6, Textual support number: 4 OBS

pilote automatique : terme uniformisé par l'Organisation de l'aviation civile internationale (OACI).  8, record 6, French, - pilote%20automatique

Record number: 6, Textual support number: 1 PHR

PA numérique.  9, record 6, French, - pilote%20automatique

Record 6,  Textual support,  Spanish

Record number: 6, Textual support number: 1 OBS

piloto automático: término aceptado oficialmente por la Organización de Aviación Civil Internacional (OACI).  2, record 6, Spanish, - piloto%20autom%C3%A1tico

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

Vertical clearances shown occur during maximum variations of airplane attitude, produced by combinations of airplane loading/unloading activities. During routine servicing, the airplane remains relatively stable, pitch and elevation changes occurring slowly.  1, record 7, English, - vertical%20clearance

Record 7,  Textual support,  French

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, 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 8, English, - standard%20rate%20turn

Record number: 8, 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 8, English, - standard%20rate%20turn

Record number: 8, 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 8, English, - standard%20rate%20turn

Record number: 8, 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 8, English, - standard%20rate%20turn

Record 8,  Textual support,  French

Record number: 8, 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 8, French, - virage%20%C3%A0%20taux%20standard

Record number: 8, 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 8, French, - virage%20%C3%A0%20taux%20standard

Record number: 8, 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 8, French, - virage%20%C3%A0%20taux%20standard

Record number: 8, 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 8, French, - virage%20%C3%A0%20taux%20standard

Record number: 8, 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 8, French, - virage%20%C3%A0%20taux%20standard

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

Embedded GPS INS. The EGI is in an all-attitude navigation system providing outputs of linear and angular acceleration, velocity, position, attitude(roll, pitch, and platform azimuth), magnetic and true heading, altitude, time tags, and time. When installed in the host platforms in the appropriate configuration, the system provides the navigation functions of the equipment it replaces. It uses vehicle electrical power(28 Vdc), turn-on and mode commands, initialization data, and altitude data, as well as Global Positioning System(GPS) satellite inputs for GPS or GPS/Inertial Navigation System(INS) operation, and is able to track five space vehicles simultaneously.  1, record 9, English, - all%2Dattitude%20navigation%20system

Record number: 9, Textual support number: 1 OBS

Attitude. The angle between an imaginary line running from the nose to the tail, and the horizontal. The attitude is judged by the level at which the horizon is seen through the canopy.  4, record 9, English, - all%2Dattitude%20navigation%20system

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 CONT

GPS et INS intégrés. Le système EGI est un système de navigation toutes attitudes qui fournit un signal d'accélération linéaire et angulaire, de vitesse, de position, d'attitude (roulis, tangage et azimut de plate-forme), un cap magnétique et vrai, l'altitude, les descripteurs temps et l'heure. Lorsqu'il est installé dans les plates-formes hôtes sous sa configuration appropriée, le système fournit les fonctions de navigation de l'équipement qu'il remplace. Il utilise le courant électrique de l'aéronef (28 V CC), les commandements de mise en marche et de mode, les données d'initialisation ainsi que les données d'altitude de même que les entrées satellites du système de positionnement global (GPS) pour le fonctionnement en GPS ou en GPS/système de navigation par inertie (INS) et peut poursuivre cinq véhicules spatiaux simultanément.  1, record 9, French, - syst%C3%A8me%20de%20navigation%20toutes%20attitudes

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 CONT

Attitude Measurement Issues. Acoustic refraction and the vessel' s roll, pitch, heading and heave determine where the acoustic beams meet the sea floor. Just asin conventional surveys, factors such as tides, storm surges and vessel draft and settlement at speed are also important in MBS [multibeam sonar] surveys. Position and heading are used to transform slant-ranges and ray angles into geo-referenced depths.  1, record 10, English, - attitude%20measurement

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 CONT

Les problèmes de mesures d’attitude. La réfraction acoustique et les mouvements du navire (roulis, tangage, cap et pilonnement) déterminent le point où les faisceaux frappent le plancher océanique. Comme pour les levés classiques, desfacteurs comme la marée, les ondes de tempête, le tirant d’eau et l’assiette dunavire en mouvement influent également sur les levés réalisés à l’aide du MBS [sonar multifaisceaux]. Laposition et le cap servent à transformer les distances obliques et les angles des rayons en valeurs de profondeurs géoréférencées.  1, record 10, French, - mesure%20d%27attitude

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 CONT

Attitude Sensor. The TSS POS/MV(Position and Orientation Systems for Marine Vessels) is an inertial navigation system delivering full 6 degree-of-freedom position and orientation systems for ships. It combines data from an inertial unit made up of three acceleration meters and three gyrolasers(fibre optic gyroscopes) and two GPS antennas. It delivers the following data with a sampling frequency of 1-200 Hz : roll and pitch(accurate to 0. 02°) ;heave(accurate to 5% amplitude) ;true heading(accurate to 0. 1°).  1, record 11, English, - attitude%20sensor

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 DEF

Ensemble des appareils servant à déterminer et à contrôler l'orientation d'un véhicule spatial.  4, record 11, French, - centrale%20d%27attitude

Record number: 11, Textual support number: 1 CONT

Des gyroscopes mécaniques à suspension dynamique, très utilisés dans les centrales à cardans, peuvent également être montés sur une centrale à composants liés, de performances plus modestes, comme une centrale d'attitude. Il s'agit d'instruments électromécaniques à masse tournante entraînée en rotation par un moteur électrique au travers d'un joint flexible qui laisse au rotor toute liberté angulaire dans les directions perpendiculaires à l'axe de rotation.  5, record 11, French, - centrale%20d%27attitude

Record number: 11, Textual support number: 2 CONT

Centrales d'attitude. La centrale TSS POS/MV (Position and Orientation Systems for Marine Vessels) désigne un système de navigation inertielle qui procure des solutions d'orientation et de positionnement à six degrés de liberté pour les navires. Elle combine les informations provenant d'une centrale inertielle constituée de trois accéléromètres et trois gyrolasers (gyroscopes à fibres optiques) et de deux antennes GPS. Elle délivre avec une fréquence d'échantillonnage 1-200 Hz les informations suivantes : roulis et tangage (précision 0.02°); pilonnement (précision 5 % de l'amplitude); cap (précision 0.1°).  6, record 11, French, - centrale%20d%27attitude

Record number: 11, Textual support number: 1 OBS

centrale d'orientation : terme publié au Journal officiel de la République française le 22 septembre 2000.  7, record 11, French, - centrale%20d%27attitude

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 OBS

... in order to trim an elevator to hold the nose down, the elevator's trim tab will actually rise up into the slipstream. The increased pressure on top of the trim tab surface caused by raising it will then deflect the entire elevator slab down slightly, causing the tail to rise and the aircraft's nose to move down. In the case of an aircraft where deployment of high-lift devices(flaps) would significantly alter the longitudinal trim, a supplementary trim tab is arranged to simultaneously deploy with the flaps so that pitch attitude is not markedly changed.  3, record 12, English, - elevator%20trim%20tab

Record number: 12, Textual support number: 2 OBS

elevator trim tab: term standardized by ISO.  4, record 12, English, - elevator%20trim%20tab

Record 12,  Textual support,  French

Record number: 12, Textual support number: 1 CONT

[...] en tangage [...] le compensateur le plus courant (quasiment indispensable) est le compensateur de profondeur, qui contrôle l'appareil sur l'axe de tangage (tendance à piquer ou à cabrer).  5, record 12, French, - compensateur%20de%20profondeur

Record number: 12, Textual support number: 1 OBS

compensateur de profondeur : terme normalisé par l'ISO.  6, record 12, French, - compensateur%20de%20profondeur

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 CONT

Limits result from the maximum pitch attitude/bank angle that can be achieved without striking the runway with the tail or with the engine pod(for underwing-mounted engines), the flaps or the wing tip...  2, record 13, English, - engine%20pod

Record number: 13, Textual support number: 1 OBS

The term "pod" should be used in non-ambiguous contexts only.  3, record 13, English, - engine%20pod

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 DEF

Ensemble constitué par un moteur d'avion et le capotage qui l'entoure.  4, record 13, French, - fuseau%2Dmoteur

Record number: 13, Textual support number: 1 OBS

La différence entre «engine nacelle» [nacelle moteur] et «engine pod» [fuseau moteur] porte sur l'endroit où l'ensemble est situé sur l'avion; la [«nacelle moteur»] est logée dans le fuselage et le [«fuseau moteur»] se trouve suspendu sous l'aile [...]  3, record 13, French, - fuseau%2Dmoteur

Record number: 13, Textual support number: 2 OBS

Utiliser le terme «fuseau» uniquement dans un contexte non ambigu.  5, record 13, French, - fuseau%2Dmoteur

Record number: 13, Textual support number: 3 OBS

fuseau moteur : terme normalisé par l'ISO.  6, record 13, French, - fuseau%2Dmoteur

Record number: 13, Textual support number: 4 OBS

fuseau moteur : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance; fuseau-moteur : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  5, record 13, French, - fuseau%2Dmoteur

Record number: 13, Textual support number: 5 OBS

fuseau-moteur : terme uniformisé par l'Organisation de l'aviation civile internationale (OACI).  7, record 13, French, - fuseau%2Dmoteur

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, 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 14, English, - shallow%20turn

Record 14,  Textual support,  French

Record number: 14, 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 14, French, - virage%20%C3%A0%20faible%20inclinaison

Record number: 14, 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 14, French, - virage%20%C3%A0%20faible%20inclinaison

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, 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 15, English, - pitch%20attitude

Record number: 15, 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 15, English, - pitch%20attitude

Record number: 15, Textual support number: 1 OBS

body attitude: term used for the B-767.  5, record 15, English, - pitch%20attitude

Record number: 15, Textual support number: 2 OBS

pitch attitude : term officially approved by the International Civil Aviation Organization(ICAO).  6, record 15, English, - pitch%20attitude

Record number: 15, Textual support number: 1 PHR

Constant pitch attitude.  7, record 15, English, - pitch%20attitude

Record 15,  Textual support,  French

Record number: 15, 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 15, French, - assiette%20en%20tangage

Record number: 15, 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 15, French, - assiette%20en%20tangage

Record number: 15, 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 15, French, - assiette%20en%20tangage

Record number: 15, 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 15, French, - assiette%20en%20tangage

Record number: 15, Textual support number: 1 PHR

Assiette longitudinale constante.  8, record 15, French, - assiette%20en%20tangage

Record 15,  Textual support,  Spanish

Record number: 15, Textual support number: 1 OBS

actitud en cabeceo : término aceptado oficialmente por la Organización de Aviación Civil Internacional (OACI).  2, record 15, Spanish, - actitud%20en%20cabeceo

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 CONT

Preprocessing is an important and diverse set of image preparation programs that act to offset problems with the band data and recalculate DN [Digital Number] values that minimize these problems. Among the programs that optimize these values are atmospheric correction(affecting the DNs of surface materials because of radiance from the atmosphere itself, involving attenuation and scattering) ;Sun illumination geometry; surface-induced geometric distortions; spacecraft velocity and attitude variations(roll, pitch, and yaw) ;effects of Earth rotation, elevation, curvature(including skew effects), abnormalities of instrument performance(irregularities of detector response and scan mode such as variations in mirror oscillations) ;loss of specific scan lines(requires destriping), and others. Once performed on the raw data, these adjustments require appropriate radiometric and geometric corrections.  2, record 16, English, - preprocessing

Record number: 16, Textual support number: 1 OBS

preprocessing: term officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  3, record 16, English, - preprocessing

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 CONT

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

Record number: 16, Textual support number: 1 OBS

prétraitement : terme uniformisé par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  3, record 16, French, - pr%C3%A9traitement

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 OBS

Embedded GPS INS. The EGI is in an all-attitude navigation system providing outputs of linear and angular acceleration, velocity, position, attitude(roll, pitch, and platform azimuth), magnetic and true heading, altitude, time tags, and time. When installed in the host platforms in the appropriate configuration, the system provides the navigation functions of the equipment it replaces.  2, record 17, English, - all%2Dattitude%20platform

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 OBS

GPS et INS intégrés. Le système EGI est un système de navigation toutes attitudes qui fournit un signal d'accélération linéaire et angulaire, de vitesse, de position, d'attitude (roulis, tangage et azimut de plate-forme), un cap magnétique et vrai, l'altitude, les descripteurs temps et l'heure. Lorsqu'il est installé dans les plates-formes hôtes sous sa configuration appropriée, le système fournit les fonctions de navigation de l'équipement qu'il remplace.  2, record 17, French, - plate%2Dforme%20gyroscopique%20toutes%20attitudes

Record number: 17, Textual support number: 2 OBS

Pluriel : des plateformes, des plates-formes.  3, record 17, French, - plate%2Dforme%20gyroscopique%20toutes%20attitudes

Record number: 17, Textual support number: 3 OBS

plateforme (sing.); plateformes (pl.) : Ces graphies, puisées des Rectifications de l'orthographe recommandées par le Conseil supérieur de la langue française, sont attestées dans le Petit Robert (2004).  4, record 17, French, - plate%2Dforme%20gyroscopique%20toutes%20attitudes

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, 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 18, English, - ISS%20attitude

Record number: 18, Textual support number: 1 OBS

ISS attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 18, English, - ISS%20attitude

Record 18,  Textual support,  French

Record number: 18, 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 18, French, - attitude%20de%20la%20Station%20spatiale

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, Textual support number: 1 CONT

The Local Vertical Local Horizontal coordinate system is referenced to the near-circular orbital plane. In order to specify the attitude of the Station with respect to the Local Vertical Local Horizontal, a system based on Eulerian angles of roll, pitch and yaw is used.  3, record 19, English, - local%20vertical%20local%20horizontal

Record number: 19, Textual support number: 2 CONT

The ISS [International Space Station] flies in an attitude that is referenced to the orbital plane of ISS using a set of local vertical/local-horizontal axes. The origin is at the ISS centre of mass, with the x-axis pointing along the direction of the orbital velocity vector (sometimes referred to as the "ram" direction). The z-axis points directly towards the Earth, and the y-axis parallel to the truss assembly ... This orientation is referred to as "x-axis toward the velocity vector" Torque Equilibrium Attitude and is the "normal" orientation of the ISS. The overall ISS design is optimised to fly in this attitude, which places the most laboratory modules in the "best" microgravity volume, supports attitude reboosts, service vehicle docking and minimises aerodynamic drag.  3, record 19, English, - local%20vertical%20local%20horizontal

Record number: 19, Textual support number: 1 OBS

local vertical local horizontal; LVLH: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 19, English, - local%20vertical%20local%20horizontal

Record 19,  Textual support,  French

Record number: 19, Textual support number: 1 OBS

local vertical local horizontal; LVLH : terme et abréviation uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  2, record 19, French, - local%20vertical%20local%20horizontal

Record 19,  Textual support,  Spanish

Record 20,  Textual support,  English

Record number: 20, Textual support number: 1 CONT

Altitude error gives incorrect distance from target and attitude error of pitch gives incorrect errors in angles of deflection and incidence...  2, record 20, English, - attitude%20error

Record 20,  Textual support,  French

Record 20,  Textual support,  Spanish

Record 21,  Textual support,  English

Record number: 21, Textual support number: 1 CONT

The Attitude and Vernier Upper Module. The Vega launch vehicle is equipped with a liquid propulsion module(AVUM), which provides roll control and pitch, yaw, and axial thrust during the final phase of flight. It shall perform the following functions :-roll control;-attitude control during coasting flight and in orbit phase;-correction of axial velocity error due to solid rocket motor performance scatter;-generation of the required velocity change for orbit circularisation(as required) ;-satellite pointing;-satellite release manoeuvres;-empty stage de-orbiting.  2, record 21, English, - attitude%20and%20Vernier%20upper%20module

Record 21,  Textual support,  French

Record number: 21, Textual support number: 1 CONT

Enfin, on attend la signature du contrat de développement du petit lanceur Vega. Il s'agit d'un lanceur composé de trois étages à propergol solide, surmonté d'un module supérieur à liquide dit AVUM (Attitude and Vernier Upper Module) - permettant le contrôle d'attitude et d'orbite, la séparation des satellites et la désorbitisation - ainsi que d'une coiffe.  2, record 21, French, - module%20sup%C3%A9rieur%20Vernier%2Fcommande%20d%27orientation

Record 21,  Textual support,  Spanish

Record 22,  Textual support,  English

Record number: 22, Textual support number: 1 CONT

The Conical Earth Sensor(CES) is a scanning horizon sensor used to gather attitude information on orbiting spacecraft. The most common application utilizes one or more CESs to provide pitch and roll attitude data for 3-axis stabilized orbiting spacecraft. The CES, a robust and a versatile sensor, can be used from low Earth orbit to above geosynchronous orbits, as well as during transfer orbits.  2, record 22, English, - scanning%20horizon%20sensor

Record 22,  Textual support,  French

Record 22,  Textual support,  Spanish

Record 23,  Textual support,  English

Record number: 23, 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 23, English, - inertial%20acceleration

Record 23,  Textual support,  French

Record number: 23, 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 23, French, - acc%C3%A9l%C3%A9ration%20inertielle

Record 23,  Textual support,  Spanish

Record 24,  Textual support,  English

Record number: 24, Textual support number: 1 CONT

Elements of a flight director indicator are :attitude indicator; fixed aircraft symbol; pitch and bank command bars; glide slope indicator...  2, record 24, English, - bank%20command%20bar

Record 24,  Textual support,  French

Record number: 24, Textual support number: 1 CONT

Un indicateur de directeur de vol comporte : un indicateur d'assiette; une maquette d'avion fixe; des barres directrices de tangage et de roulis; un indexe d'alignement de descente [...]  3, record 24, French, - barre%20directrice%20de%20roulis

Record 24,  Textual support,  Spanish

Record 25,  Textual support,  English

Record number: 25, Textual support number: 1 CONT

Elements of a flight director indicator are :attitude indicator; fixed aircraft symbol; pitch and bank command bars; glide slope indicator; localizer deviation indicator; slip indicator; warning flag for gyro, computer and glide slope.  1, record 25, English, - pitch%20command%20bar

Record 25,  Textual support,  French

Record number: 25, Textual support number: 1 CONT

Un indicateur de directeur de vol comporte : un indicateur d'assiette; une maquette d'avion fixe; des barres directrices de tangage et de roulis; un index d'alignement de descente; un index d'écart d'alignement de piste; un indicateur de glissade-dérapage; des drapeaux d'alarme gyro, calculateur et alignement de descente.  1, record 25, French, - barre%20directrice%20de%20tangage

Record 25,  Textual support,  Spanish

Record 26,  Textual support,  English

Record number: 26, Textual support number: 1 DEF

The orientation of an aircraft’s axes in relation to some plane, especially the horizontal.  2, record 26, English, - attitude

Record number: 26, Textual support number: 1 CONT

The attitude of an aircraft....is define d by the angles made by its axes with the relative airflow, or with the ground, respectively  2, record 26, English, - attitude

Record number: 26, Textual support number: 1 OBS

This term has been lifted straight from aeronautics and applies to the body of a car relative to the ground in the same way as with an aircraft ...  2, record 26, English, - attitude

Record number: 26, Textual support number: 2 OBS

... if using the term "attitude", beware the misleadingly similar term "attitude angle", which refers to an angle in yaw and not in pitch.  2, record 26, English, - attitude

Record 26,  Textual support,  French

Record number: 26, Textual support number: 1 DEF

Position d'équilibre des ressorts de suspension d'un véhicule par rapport au sol.  2, record 26, French, - attitude

Record number: 26, Textual support number: 1 OBS

Si on a été amené à contrebraquer, lors de sa remise en ligne, les suspensions écrasées durant tout le virage retrouvent brutalement leur assiette si l'on ne s'y est pas préparé, c'est le tête à queue garanti.  2, record 26, French, - attitude

Record 26,  Textual support,  Spanish

Record 27,  Textual support,  English

Record number: 27, 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 27, English, - inertial%20reference

Record 27,  Textual support,  French

Record number: 27, 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 27, French, - r%C3%A9f%C3%A9rence%20inertielle

Record number: 27, 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 27, French, - r%C3%A9f%C3%A9rence%20inertielle

Record 27,  Textual support,  Spanish

Record 28,  Textual support,  English

Record number: 28, 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 28, English, - natural%20horizon

Record number: 28, 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 28, English, - natural%20horizon

Record number: 28, 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 28, English, - natural%20horizon

Record 28,  Textual support,  French

Record number: 28, 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 28, French, - horizon%20naturel

Record number: 28, 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 28, French, - horizon%20naturel

Record number: 28, 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 28, French, - horizon%20naturel

Record number: 28, 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 28, French, - horizon%20naturel

Record 28,  Textual support,  Spanish

Record 29,  Textual support,  English

Record number: 29, Textual support number: 1 CONT

United States Air Force Manual 51-37, Instrument Flying,... categorizes flight instruments into three functional groups : control, performance, and navigation. In the control category are the parameters of aircraft attitude(i. e., pitch and bank} and engine power or thrust. In the performance category are airspeed, altitude, vertical velocity, heading, turn rate, slip/skid rate, angle of attack, acceleration(G loading), and flight path(velocity vector).  3, record 29, English, - skid%20rate

Record number: 29, Textual support number: 1 OBS

skid: An uncoordinated maneuver which results from too much rudder (or not enough aileron ...) in a turn. Compare to slip... Slip: An uncoordinated maneuver ... which results from too little rudder in a turn.  4, record 29, English, - skid%20rate

Record 29,  Textual support,  French

Record number: 29, Textual support number: 1 OBS

L'horizon artificiel [...] sert à indiquer la position d'un avion par rapport à l'horizon terrestre symbolisé par une ligne séparant deux zones de couleurs différentes, l'une indiquant le ciel, l'autre la terre. L'attitude de l'avion est déduite de la position de cette ligne qui fournit des précisions sur le roulis et le tangage. Des marques sur les côtés précisent le degré d'inclinaison de l'avion et une bille située dans la partie inférieure informe le pilote du [taux de dérapage].  2, record 29, French, - taux%20de%20d%C3%A9rapage

Record 29,  Textual support,  Spanish

Record 30,  Textual support,  English

Record number: 30, 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 30, English, - pitch%20gimbal

Record 30,  Textual support,  French

Record number: 30, 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 30, French, - cadre%20de%20tangage

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, - roll%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%20roulis

Record 31,  Textual support,  Spanish

Record 32,  Textual support,  English

Record number: 32, Textual support number: 1 DEF

An error in gyro output due to cross-coupling and acceleration encountered during vehicle turns.  3, record 32, English, - turn%20error

Record number: 32, Textual support number: 1 CONT

Principal Attitude Indicator Errors. Turn Error. During a normal coordinated turn, centrifugal force causes the gyro to precess toward the inside of the turn. This precession increases as the bank steepens; therefore, it is greatest during the actual turn. The error disappears as the aircraft rolls out at the end of a 180 degrees turn at a normal rollout rate. Therefore, when performing a steep turn, the pilot may use the attitude indicator for rolling in and out of the turn, but should use other instruments(VSI and altimeter) during the turn for specific pitch information.  4, record 32, English, - turn%20error

Record 32,  Textual support,  French

Record 32,  Textual support,  Spanish

Record 33,  Textual support,  English

Record number: 33, 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 33, English, - roll%20component

Record number: 33, 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 33, English, - roll%20component

Record 33,  Textual support,  French

Record number: 33, 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 33, French, - composante%20en%20roulis

Record number: 33, 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 33, French, - composante%20en%20roulis

Record 33,  Textual support,  Spanish

Record 34,  Textual support,  English

Record number: 34, 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 34, English, - pitch%20component

Record number: 34, 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 34, English, - pitch%20component

Record 34,  Textual support,  French

Record number: 34, 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 34, French, - composante%20en%20tangage

Record number: 34, 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 34, French, - composante%20en%20tangage

Record 34,  Textual support,  Spanish

Record 35,  Textual support,  English

Record number: 35, 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 35, English, - two%20degree%20of%20freedom%20VG

Record 35,  Textual support,  French

Record number: 35, 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 35, French, - gyroscope%20de%20verticale%20%C3%A0%20deux%20degr%C3%A9s%20de%20libert%C3%A9

Record 35,  Textual support,  Spanish

Record 36,  Textual support,  English

Record number: 36, 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 36, English, - gyroscopic%20heading%20and%20attitude%20reference%20system

Record 36,  Textual support,  French

Record number: 36, 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 36, French, - centrale%20gyroscopique%20de%20cap%20et%20de%20verticale

Record 36,  Textual support,  Spanish

Record 37,  Textual support,  English

Record number: 37, 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 37, English, - Station%26rsquo%3Bs%20flight%20attitude

Record number: 37, Textual support number: 1 OBS

Station’s flight attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 37, English, - Station%26rsquo%3Bs%20flight%20attitude

Record 37,  Textual support,  French

Record number: 37, 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 37, French, - attitude%20de%20la%20Station

Record number: 37, 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 37, French, - attitude%20de%20la%20Station

Record 37,  Textual support,  Spanish

Record 38,  Textual support,  English

Record number: 38, 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 38, English, - environmental%20torque

Record 38,  Textual support,  French

Record 38,  Textual support,  Spanish

Record 39,  Textual support,  English

Record number: 39, 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 39, English, - attitude%20hold

Record 39,  Textual support,  French

Record 39,  Textual support,  Spanish

Record 40,  Textual support,  French

Record 40,  Textual support,  Spanish

Record 41,  Textual support,  English

Record number: 41, Textual support number: 1 CONT

The flight guidance computer only operates or three cue(pitch, roll and collective) attitude director in the 212.  1, record 41, English, - three%2Dcue%20attitude%20director

Record 41,  Textual support,  French

Record 41,  Textual support,  Spanish

Record 42,  Textual support,  English

Record number: 42, 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 42, English, - jerky%20engagement

Record 42,  Textual support,  French

Record number: 42, 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 42, French, - r%C3%A9actions%20brusques%20%C3%A0%20l%27engagement

Record 42,  Textual support,  Spanish

Record 43,  Textual support,  English

Record number: 43, Textual support number: 1 OBS

The pitch and roll sphere displays the pitch and roll attitude of the aircraft from a fixed miniature aircraft.  1, record 43, English, - pitch%20and%20roll%20sphere

Record 43,  Textual support,  French

Record number: 43, Textual support number: 1 OBS

(...) il faut voler de façon à amener les aiguilles [du directeur de vol] au centre de l'indicateur. Ceci réalisé signifie: - que l'avion est dans les conditions de vol prévues auquel cas l'horizon artificiel sphérique est lui-même bien centré en tangage et roulis.  1, record 43, French, - horizon%20artificiel%20sph%C3%A9rique

Record number: 43, Textual support number: 2 OBS

Le code de source complet est INCAR-SE-210,1971,34-23-10,1  2, record 43, French, - horizon%20artificiel%20sph%C3%A9rique

Record 43,  Textual support,  Spanish

Record 44,  Textual support,  English

Record number: 44, Textual support number: 1 OBS

Two identical INS's [inertial navigation sets](No. 1 and No. 2) supply the FDS [flight director set] with pitch and roll attitude and waypoint steering signals.  1, record 44, English, - waypoint%20steering%20signal

Record 44,  Textual support,  French

Record 44,  Textual support,  Spanish

Record 45,  Textual support,  English

Record number: 45, Textual support number: 1 CONT

The... switchlight is used by the copilot to select either INS No. 2 or the standby attitude indicator as the source of pitch and roll attitude to the flight director computer... and copilot's FDI sphere.  1, record 45, English, - attitude%20source

Record 45,  Textual support,  French

Record number: 45, Textual support number: 1 CONT

Sur les avions de ligne on répétera [...] les informations principales : altitude, vitesse, etc. sur les planches pilote et copilote. Poussant plus loin la sécurité, on cherchera à ce que ces informations soient le plus indépendantes possibles : centrales anémométriques distinctes, sources de cap ou d'assiette distinctes.  1, record 45, French, - source%20d%27assiette

Record 45,  Textual support,  Spanish

Record 46,  Textual support,  English

Record 46,  Textual support,  French

Record number: 46, Textual support number: 1 OBS

terme d'usage obligatoire au Bureau des Traductions.  2, record 46, French, - signaux%20d%27assiette

Record 46,  Textual support,  Spanish

Record 47,  Textual support,  English

Record 47,  Textual support,  French

Record number: 47, Textual support number: 1 OBS

terme d'usage obligatoire au Bureau des Traductions.  2, record 47, French, - assiette%20pr%C3%A9%C3%A9tablie

Record 47,  Textual support,  Spanish

Record 48,  Textual support,  English

Record 48,  Textual support,  French

Record number: 48, Textual support number: 1 OBS

terme d'usage obligatoire au Bureau des Traductions.  2, record 48, French, - assiette%20%C3%A0%20piquer

Record 48,  Textual support,  Spanish

Record 49,  Textual support,  French

Record 49,  Textual support,  Spanish

Record 50,  Textual support,  French

Record 50,  Textual support,  Spanish