TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 DEF

The regulation of the attitude of [a] spacecraft ...  3, record 1, English, - attitude%20control

Record number: 1, Textual support number: 1 CONT

The attitude of a spacecraft is defined as the direction the spacecraft is pointing with respect to some inertial reference frame. The control of this attitude is a complex but essential task that all spacecraft must somehow perform in order to orient instrumentations, antennas, solar panels, and more. Attitude control is divided into two primary tasks :(1) the determination or measurement of the attitude and(2) the ability to control the direction the spacecraft is pointing.  4, record 1, English, - attitude%20control

Record number: 1, Textual support number: 1 OBS

attitude control; ACTL: term and abbreviation officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  2, record 1, English, - attitude%20control

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 DEF

Action d’imposer l’orientation voulue à un engin spatial.  5, record 1, French, - commande%20d%27orientation

Record number: 1, Textual support number: 1 OBS

ACTL : acronyme spécifique à Radarsat.  6, record 1, French, - commande%20d%27orientation

Record number: 1, Textual support number: 2 OBS

commande d'orientation : terme et définition publiés au Journal officiel de la République française le 25 juillet 2015.  7, record 1, French, - commande%20d%27orientation

Record number: 1, Textual support number: 3 OBS

commande d'attitude; ACTL : terme et abréviation uniformisés par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  6, record 1, French, - commande%20d%27orientation

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, 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 2, English, - attitude%20measurement

Record 2,  Textual support,  French

Record number: 2, 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 2, French, - mesure%20d%27attitude

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

Three orthogonal gyros measure the rate of rotation of the satellite. Two options : Always on-good measurement of attitude, but drifts so needs to be reset occasionally. Turn on with other devices-can only measure instantaneous rotation rates.  1, record 3, English, - instantaneous%20rotation

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 CONT

Gyrométrie optique [...] Considérons un observateur [...] se trouvant à bord d'un laboratoire (ou d'un véhicule) en mouvement par rapport à l'espace absolu. Deux procédés s'offrent à lui pour mesurer la rotation instantanée de ce laboratoire : la mécanique rationnelle et l'optique. Mécanique rationnelle : par l'existence des forces d'inerties [...] cette voie conduit à la réalisation de gyromètres mécaniques [...] Optique : cette voie, par l'influence de la rotation du laboratoire (et par la suite des instruments utilisés) sur l'interaction instrument-lumière, conduit à la réalisation des gyromètres à fibres optiques et à celle des gyromètres laser.  2, record 3, French, - rotation%20instantan%C3%A9e

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

The Attitude Sensor Package(ASP), mounted in the cargo bay, will demonstrate three new spacecraft attitude sensors in order to establish confidence in their accuracy and functional performance. The three sensors use various techniques including star tracking, Earth limb/deep space temperature differences, and velocity vector measurement.  3, record 4, English, - attitude%20sensor%20package

Record 4,  Textual support,  French

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 CONT

In order to sustain the required technological development, ESA issued two Invitations To Tender on Active Pointing of Large Telescopes(APLT) and Attitude Measurement Transfer System(AMTS), awarded to a proposal led by Alenia Spazio(Prime Contractor).  2, record 5, English, - attitude%20measurement%20transfer%20system

Record 5,  Textual support,  French

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 CONT

The Attitude Measurement Electronics uses inputs from the spacecraft Sun Sensors, Attitude and Orbit Control Electronics(AOCE) and ground commands to provide the spacecraft subsystems with refined Sun pulse information, and to control the position of the fuel regulation valves and heaters in the Reaction Control Subsystem. It also takes power from the AOCS power converters and provides power switching for other units within the AOCS.  2, record 6, English, - attitude%20measurement%20electronics

Record 6,  Textual support,  French

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

Throughout rapid align[ment] the electronic circuits which normally drive the gyro torque motors are used to process the error signals required to align the platform.  1, record 7, English, - gyro%20torque%20motor

Record number: 7, Textual support number: 1 OBS

Torque motor. A motor that receives information from the frames in the inertial measurement unit about changes in attitude of a rocket or missile [or aircraft], which in turn helps to correct the attitude of the rocket or missile [or aircraft], as needed.  2, record 7, English, - gyro%20torque%20motor

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 CONT

Au cours de l'alignement rapide, les circuits électroniques qui entraînent normalement les moteurs couples du gyroscope sont utilisés pour traiter les signaux d'erreur requis pour aligner la plate-forme.  1, record 7, French, - moteur%20couple%20du%20gyro

Record number: 7, Textual support number: 1 OBS

Gyroscopes libres [...] Ils comportent souvent [...] des «moteurs-couples», permettant d'appliquer à la toupie des couples connus, dans le but de compenser certains couples perturbateurs ou encore d'obtenir de la toupie une précession déterminée.  2, record 7, French, - moteur%20couple%20du%20gyro

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

In its simplest form, an inertial navigation system(INS) consists of an inertial measurement unit(IMU), the navigation computer, and a computer interface. Therefore, the inertial navigation system aboard an aircraft provides, through self-contained equipment, aircraft acceleration, velocity, position, attitude, and heading to the onboard navigation computer and other aircraft subsystems... For certain operations and/or missions... dual or triple redundant inertial navigation systems are required... In a dual INS configuration... as long as either inertial navigation system is providing valid data, its output can be used as the primary reference source for the navigation subsystem.  1, record 8, English, - dual%20redundant%20inertial%20navigation%20system

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 OBS

Le Grippen dispose d'un système de commande de vol électrique digitale à triple redondance et d'une centrale inertielle Honeywell.  2, record 8, French, - syst%C3%A8me%20de%20navigation%20inertielle%20%C3%A0%20double%20redondance

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

In its simplest form, an inertial navigation system(INS) consists of an inertial measurement unit(IMU), the navigation computer, and a computer interface. Therefore, the inertial navigation system aboard an aircraft provides, through self-contained equipment, aircraft acceleration, velocity, position, attitude, and heading to the onboard navigation computer and other aircraft subsystems... For certain operations and/or missions... dual or triple redundant inertial navigation systems are required.... In a dual INS configuration... as long as either inertial navigation system is providing valid data, its output can be used as the primary reference source for the navigation subsystem.  1, record 9, English, - triple%20redundant%20inertial%20navigation%20system

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 OBS

Le Grippen dispose d'un système de commande de vol électrique digitale à triple redondance et d'une centrale inertielle Honeywell.  2, record 9, French, - syst%C3%A8me%20de%20navigation%20inertielle%20%C3%A0%20triple%20redondance

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 CONT

The VG400CA is a high performance, solid-state vertical gyro intended for airborne applications such as UAV control, avionics, and platform stabilization. This high reliability, strap-down inertial subsystem provides attitude measurement with static and dynamic accuracy comparable to traditional spinning mass vertical gyros.  1, record 10, English, - solid%2Dstate%20vertical%20gyro

Record number: 10, Textual support number: 1 OBS

solid state technology: A general term for sensors that do not have moving parts.  2, record 10, English, - solid%2Dstate%20vertical%20gyro

Record number: 10, Textual support number: 2 OBS

solid state: Pertaining to a circuit, device, or system that depends on some combination of electrical, magnetic, and optical phenomena within a solid that is usually a crystalline semiconductor material.  3, record 10, English, - solid%2Dstate%20vertical%20gyro

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 OBS

Les gyroscopes vibrants représentent aujourd'hui une nouvelle et importante technologie inertielle, non seulement parce que, pour certains d'entre eux, ils on montré leur capacité à être très performants (on dit alors qu'ils sont de classe inertielle), mais que, surtout, dans les autres technologies dites «solid-state» [semiconducteurs] (gyroscopes laser et à fibre optique), les gyroscopes n'ont pas la même aptitude que les gyroscopes vibrants à être miniaturisés et fabriqués à des coûts faibles.  2, record 10, French, - gyroscope%20de%20verticale%20%C3%A0%20semi%2Dconducteur

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 CONT

The VG400CA is a high performance, solid-state vertical gyro intended for airborne applications such as UAV control, avionics, and platform stabilization. This high reliability, strap-down inertial subsystem provides attitude measurement with static and dynamic accuracy comparable to traditional spinning mass vertical gyros.  1, record 11, English, - spinning%20mass%20vertical%20gyro

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 OBS

[...] les systèmes inertiels se composent d'un minimum de deux gyroscopes, chacun desquels supporte une masse globulaire placée à l'intérieur d'un cardan. [...] Nous savons [...] que l'axe de l'objet qui tourne présente une verticale parfaite. S'il y a inclinaison de la plate-forme, comme par exemple lors d'un virage sur l'aile, le cardan s'incline en tandem avec l'avion tandis que la masse tournante demeure à la verticale. On peut dès lors mesurer l'angle d'inclinaison.  2, record 11, French, - gyroscope%20de%20verticale%20%C3%A0%20masse%20tournante

Record number: 11, Textual support number: 2 OBS

Sur certains gyroscopes perfectionnés, des cercles divisés permettent de relever avec précision la position de la masse rotative, de sorte qu'on peut, avec cet instrument, déterminer la position du plan méridien, celle de l'axe du monde, et par suite, la latitude.  3, record 11, French, - gyroscope%20de%20verticale%20%C3%A0%20masse%20tournante

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 DEF

A coordinate system in which a body moves with constant velocity as long as no force is acting on it.  3, record 12, English, - inertial%20coordinate%20frame

Record number: 12, Textual support number: 1 CONT

In its simplest form, an inertial navigation system(INS) consists of an inertial measurement unit(IMU), the navigation computer, and a computer interface. Therefore, the inertial navigation system aboard an aircraft provides... aircraft acceleration, velocity, position, attitude, and heading to the onboard navigation computer... The IMU... measures the specific force and attitude of the vehicle in an inertial coordinate frame. These inertial coordinates are in turn transferred to the computer, which determines the vehicle position in the desired reference frame.  4, record 12, English, - inertial%20coordinate%20frame

Record 12,  Textual support,  French

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 DEF

A computer that uses electronic or electric circuits to compute two or more navigation factors such as altitude, direction, and velocity, or to receive such data and compute course information.  4, record 13, English, - navigation%20computer

Record number: 13, Textual support number: 1 CONT

In its simplest form, an inertial navigation system(INS) consists of an inertial measurement unit(IMU), the navigation computer, and a computer interface. Therefore, the inertial navigation system aboard an aircraft provides, through self-contained equipment, aircraft acceleration, velocity position, attitude, and heading to the onboard navigation computer and other aircraft subsystems... in a convenient coordinate frame.  2, record 13, English, - navigation%20computer

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 CONT

Le programme de modernisation MirSIP des Mirages 5 est attribué à la SABCA qui travaillera en étroite collaboration avec Dassault Aviation. Il est axé principalement sur la sécurité de l'avion et sur d'autres modifications, notamment: [...] L'installation d'un système de navigation, de tir et de reconnaissance très moderne comprenant : Un télémètre laser, installé sous le nez de l'avion. La plateforme de navigation inertielle du F-16. Un calculateur de navigation et d'attaque, muni d'un écran cathodique [...]  3, record 13, French, - calculateur%20de%20navigation

Record number: 13, Textual support number: 2 CONT

Le calculateur de bombardement devait [...] déterminer en fonction des conditions de vol instantanées, le point de chute futur de la bombe, si elle était larguée à cet instant. À partir de cette donnée, constamment remise à jour, le calculateur de navigation devait donner au pilote automatique les ordres pour amener ce point à coïncider avec le but et commander automatiquement le largage de la bombe lorsque cette coïncidence était réalisée, en fournissant pour information de l'équipage le décompte des dix dernières secondes.  4, record 13, French, - calculateur%20de%20navigation

Record number: 13, Textual support number: 1 OBS

calculateur de navigation : terme d'usage obligatoire au Bureau de la traduction.  5, record 13, French, - calculateur%20de%20navigation

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 DEF

A rigid platform stabilized with respect to inertial space (through the use of attitude reference gyroscopes and servo loops) to which are mounted accelerometers.  3, record 14, English, - inertial%20measurement%20unit

Record number: 14, Textual support number: 1 CONT

The Inertial Measurement Units(IMUs) are an important part of the navigation system of the Space Shuttle. They provide attitude and velocity state information with respect to a known inertial coordinate reference. Three identical and functionally independent IMU's are flown on board each orbiter.  4, record 14, English, - inertial%20measurement%20unit

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 DEF

mesureur inertiel : Appareil permettant de mesurer l'accélération et de calculer la position d'un engin spatial lorsqu'on a recours au guidage par inertie.  3, record 14, French, - unit%C3%A9%20de%20mesure%20inertielle

Record number: 14, Textual support number: 1 CONT

Le GNCS [Guidance, Navigation and Control System] est une combinaison de senseurs optiques, de gyroscopes et d'un ordinateur, destinés à mesurer l'attitude et la vitesse du vaisseau, ainsi que sa position dans l'espace [...] [Il] est divisé en 3 sous-systèmes : Inertiel (Inertial Subsystem, ISS). L'organe majeur de l'ISS est l'unité de mesure inertielle [...], qui fournit une plate-forme inertielle fixe. Peu importe la position du vaisseau, la plate-forme stable de l'IMU reste fixe, comme la surface de l'eau dans un verre. Dès qu'une variation est détectée, un IRIG (Inertial Rate Integrating Gyroscope) rétablit l'orientation de la plate-forme. [...] Optique (Optical Subsystem, OSS). [...] Informatique (Computer Subsystem, CSS).  4, record 14, French, - unit%C3%A9%20de%20mesure%20inertielle

Record number: 14, Textual support number: 2 CONT

Les centrales inertielles d'Ariane 5. [...] Cette centrale à composants liés comprend une unité de mesure inertielle, avec trois gyrolasers de 33 cm de périmètre et trois accéléromètres de précision, ainsi qu'une unité de traitement de données. Elle sert au guidage du lanceur et à la surveillance des paramètres de vol.  5, record 14, French, - unit%C3%A9%20de%20mesure%20inertielle

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 CONT

In its simplest form, an inertial navigation system(INS) consists of an inertial measurement unit(IMU), the navigation computer, and a computer interface. Therefore, the inertial navigation system aboard an aircraft provides, through self-contained equipment, aircraft acceleration, velocity, position, attitude, and heading to the onboard navigation computer and other aircraft subsystems... For certain operations and/or missions... dual or triple redundant inertial navigation systems are required... In a dual INS configuration... as long as either inertial navigation system is providing valid data, its output can be used as the primary reference source for the navigation subsystem.  1, record 15, English, - dual%20INS%20configuration

Record 15,  Textual support,  French

Record number: 15, Textual support number: 1 OBS

Le Grippen dispose d'un système de commande de vol électrique digitale à triple redondance et d'une centrale inertielle Honeywell.  2, record 15, French, - configuration%20navigation%20inertielle%20%C3%A0%20double%20redondance

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 CONT

Attitude measurement includes measurement of the consumer's overall affective evaluation(like-dislike), as well as factors that influence this overall evaluation(importance and brand beliefs) and results of the attitude(behavioral intention).  1, record 16, English, - attitude%20measurement

Record 16,  Textual support,  French

Record 16,  Textual support,  Spanish