TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

In the bob-up manoeuvre, Smith explained that information from the Doppler, the HARS(Heading and Attitude Reference System) and air data sensor are fed to the computer, which then maintains the hover in an eight-foot square and gives a velocity vector.  1, record 1, English, - bob%2Dup%20manoeuvre

Record 1,  Textual support,  French

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

Inertial platform... Stable platforms utilizing gyroscopes references have been successfully used for several decades as attitude and heading reference systems(AHRS), fire control baselines for aircraft, ships, missiles, and for inertial navigators. The part of the platform system, which mechanizes the reference is called "controlled member" or "stable element".  2, record 2, English, - controlled%20member

Record number: 2, Textual support number: 2 CONT

For a three-gimbal platform ... the inner gimbal or controlled member is the stable platform on which the three gyros and accelerometers are mounted. As the vehicle to which the system is attached moves, the gyros sense any rotation and drive the gimbals in the opposite direction to null the gyro rate. As a result, the inner platform remains fixed in inertial space.  5, record 2, English, - controlled%20member

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 CONT

On distingue deux types de systèmes inertiels : - Les systèmes sur cardans, dont la plate-forme contenant les accéléromètres est montée sur les cardans internes de trois gyroscopes. La plate-forme est isolée de toute rotation du véhicule et son attitude reste constante pendant le mouvement du système. Ces dispositifs complexes sont précis, mais complexes et onéreux. - Les systèmes dits «strap-down», qui utilisent des accéléromètres et des gyroscopes soumis aux mouvements du véhicule. Ces systèmes sont plus simples à mettre en œuvre, moins chers mais moins précis.  1, record 2, French, - cardan%20interne

Record number: 2, Textual support number: 2 CONT

Le gyroscope de Foucault est une toupie rectifiée [...] formée d'une masse de cuivre [...] montée sur un axe dont les deux extrémités sont fixées sur un anneau lui-même suspendu aux deux extrémités du diamètre perpendiculaire à celui de l'axe qui porte la masse de cuivre, de sorte que celle-ci peut prendre toutes les inclinaisons possibles sur l'horizon. Les deux pivots de ce premier anneau reposent sur un deuxième anneau plus grand, monté lui-même sur pivots lui permettant une rotation verticale. [...] Si on fixe horizontalement l'anneau intérieur, l'axe de rotation ne pourra plus se déplacer que dans un plan horizontal.  3, record 2, French, - cardan%20interne

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

The attitude heading reference system provides attitude gyro, directional gyro(compass) and 3-axis rate/accelerometer data to the following aeroplane systems in EFIS [electronic flight instrument system] equipped aircraft : Primary flight and multi-function displays; Weather radar system; Automatic Flight Control System; Ground Proximity Warning System; Traffic Alert and Collision Avoidance System; Stall Protection System; Fuel System; Flight Data Recorder; Body Rates and Linear Acceleration Data to the flight control system.  13, record 3, English, - attitude%20and%20heading%20reference%20system

Record number: 3, Textual support number: 2 CONT

Crossbow [TM] Technology, Inc.... introduced its new AHRS500GA solid-state attitude and heading reference system for general aviation... Crossbow's AHRS500GA is a strap-down subsystem that delivers heading measurements with dynamic accuracy of +/-2. 0 and static accuracy of +/-1. 5. Attitude accuracy is less than +/-0. 5 degrees(static) and +/-2. 0 degrees(dynamic). Range is +/-180 degrees. The system features the industry's highest performing sensors, including advanced MEMs accelerometers and rate gyros that provide much higher reliability than traditional spinning mass gyros.  14, record 3, English, - attitude%20and%20heading%20reference%20system

Record number: 3, Textual support number: 1 OBS

heading and attitude reference system; HARS : term and abbreviation officialized by the Aeronautical Terminology Standardization Committee(ATSC)-Helicopters.  15, record 3, English, - attitude%20and%20heading%20reference%20system

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 CONT

Une centrale moderne d'attitude et de cap [...] ressemble beaucoup à une centrale inertielle de navigation qui ne fournirait que les assiettes et le cap, et dont les gyroscopes et les accéléromètres seraient de performances modestes : 1 à 10 degrés par heure pour les gyroscopes et quelques millièmes de la pesanteur pour les accéléromètres. La centrale d'attitude et de cap peut être à cardans ou à composants liés [...] et utiliser des gyroscopes mécaniques ou des gyrolasers.  2, record 3, French, - centrale%20d%27attitude%20et%20de%20cap

Record number: 3, Textual support number: 1 OBS

centrale de cap et de verticale; AHRS : terme et abréviation uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  9, record 3, French, - centrale%20d%27attitude%20et%20de%20cap

Record number: 3, Textual support number: 2 OBS

centrale de cap et d'attitude : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Hélicoptères.  10, record 3, French, - centrale%20d%27attitude%20et%20de%20cap

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

Synchro signal amplifier(CRA-3). The CRA-3 is designed to operate with GHARS [gyroscopic heading and attitude reference system], and other compass systems... The unit may be used for multiple bearing and other repeater applications. The CRA-3 consists of a transistor amplifier, control transformer and motor with gear head designed to drive four size eleven high power synchro torque transmitters, a synchro differential and two resolvers each of which may be excited separately. Each synchro torque transmitter is capable of driving up to four high torque synchro receivers.  1, record 4, English, - high%20power%20synchro%20torque%20transmitter

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 CONT

Synchro amplificateur de signaux (CRA-3). Le CRA-3 est conçu pour fonctionner avec la centrale gyroscopique de cap et de verticale et d'autres systèmes de compas [...] Le CRA-3 se compose d'un amplificateur transistorisé, d'un transformateur de commande et d'un moteur avec train d'engrenages conçu pour entraîner quatre synchro transmetteurs de couple à puissance élevée de grandeur onze, un synchro différentiel et deux résolvers, pouvant tous être excités séparément. Chaque synchro transmetteur de couple est capable d'entraîner jusqu'à quatre synchro récepteurs à couple élevé.  1, record 4, French, - synchro%20transmetteur%20de%20couple%20%C3%A0%20puissance%20%C3%A9lev%C3%A9e

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, 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 5, English, - dual%20redundant%20inertial%20navigation%20system

Record 5,  Textual support,  French

Record number: 5, 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 5, French, - syst%C3%A8me%20de%20navigation%20inertielle%20%C3%A0%20double%20redondance

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, 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 6, English, - triple%20redundant%20inertial%20navigation%20system

Record 6,  Textual support,  French

Record number: 6, 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 6, French, - syst%C3%A8me%20de%20navigation%20inertielle%20%C3%A0%20triple%20redondance

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

Culminating a decade of pace-setting LITEF fiber optic gyro(FOG) research and development, the LCR-92 µ-AHRS strapdown Attitude and Heading Reference System... offers near-inertial quality heading and attitude capability at a price and with the reliability that today's business aviation and regional airline operators demand. It is a cost-effective replacement for expensive-to-maintain gimballed attitude-directional-and rate-gyro-based systems, priced competitively with that 1960's technology but with up to five times the Mean Time Between Failure(MTBF). And it is smaller, lighter, and significantly less costly than other fiber optic gyro-based AHRS.  4, record 7, English, - strapdown%20attitude%20and%20heading%20reference%20system

Record number: 7, Textual support number: 1 OBS

strapdown: A term used to describe inertial measurement instruments (gyroscopes, accelerometers, and VMs) that are not mounted on a stable inertial platform but directly on the vehicle itself.  5, record 7, English, - strapdown%20attitude%20and%20heading%20reference%20system

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 CONT

Une centrale moderne d'attitude et de cap [...] ressemble beaucoup à une centrale inertielle de navigation qui ne fournirait que les assiettes et le cap, et dont les gyroscopes et les accéléromètres seraient de performances modestes : 1 à 10 degrés par heure pour les gyroscopes et quelques millièmes de la pesanteur pour les accéléromètres. La centrale d'attitude et de cap peut être à cardans ou à composants liés (strap down) et utiliser des gyroscopes mécaniques ou des gyrolasers.  1, record 7, French, - centrale%20d%27attitude%20et%20de%20cap%20%C3%A0%20composants%20li%C3%A9s

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

Synchro signal amplifier(CRA-3). The CRA-3 is designed to operate with GHARS [gyroscopic heading and attitude reference system], and other compass systems... The unit may be used for multiple bearing and other repeater applications. The CRA-3 consists of a transistor amplifier, control transformer and motor with gear head designed to drive four size eleven high power synchro torque transmitters, a synchro differential and two resolvers each of which may be excited separately.  1, record 8, English, - control%20transformer

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 CONT

Synchro-amplificateur de signaux (CRA-3). Le CRA-3 est conçu pour fonctionner avec la centrale gyroscopique de cap et de verticale et d'autres systèmes de compas [...] Le CRA-3 se compose d'un amplificateur transistorisé, d'un transformateur de commande et d'un moteur avec train d'engrenages conçu pour entraîner quatre synchro-transmetteurs de couple à puissance élevée de grandeur onze, un synchro-différentiel et deux résolvers, pouvant tous être excités séparément.  1, record 8, French, - transformateur%20de%20commande

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 CONT

Synchro signal amplifier(CRA-3). The CRA-3 is designed to operate with GHARS [gyroscopic heading and attitude reference system], and other compass systems.... The unit may be used for multiple bearing and other repeater applications. The CRA-3 consists of a transistor amplifier, control transformer and motor with gear head designed to drive four size eleven high power synchro torque transmitters, a synchro differential and two resolvers each of which may be excited separately. Each synchro torque transmitter is capable of driving up to four high torque synchro receivers.  3, record 9, English, - synchro%20torque%20transmitter

Record number: 9, Textual support number: 2 CONT

Synchro torque transmitter. The synchro transmitter converts the angular position of its rotor (mechanical input) into an electrical output signal.  2, record 9, English, - synchro%20torque%20transmitter

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 CONT

Synchro amplificateur de signaux (CRA-3). Le CRA-3 est conçu pour fonctionner avec la centrale gyroscopique de cap et de verticale et d'autres systèmes de compas [...] Le CRA-3 se compose d'un amplificateur transistorisé, d'un transformateur de commande et d'un moteur avec train d'engrenages conçu pour entraîner quatre synchro transmetteurs de couple à puissance élevée de grandeur onze, un synchro différentiel et deux résolvers, pouvant tous être excités séparément. Chaque synchro transmetteur de couple est capable d'entraîner jusqu'à quatre synchro récepteurs à couple élevé.  1, record 9, French, - synchro%20transmetteur%20de%20couple

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 CONT

Synchro signal amplifier(CRA-3). The CRA-3 is designed to operate with GHARS [gyroscopic heading and attitude reference system], and other compass systems... The unit may be used for multiple bearing and other repeater applications. The CRA-3 consists of a transistor amplifier, control transformer and motor with gear head designed to drive four size eleven high power synchro torque transmitters, a synchro differential and two resolvers each of which may be excited separately. Each synchro torque transmitter is capable of driving up to four high torque synchro receivers.  1, record 10, English, - high%20torque%20synchro%20receiver

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 CONT

Synchro amplificateur de signaux (CRA-3). Le CRA-3 est conçu pour fonctionner avec la centrale gyroscopique de cap et de verticale et d'autres systèmes de compas [...] Le CRA-3 se compose d'un amplificateur transistorisé, d'un transformateur de commande et d'un moteur avec train d'engrenages conçu pour entraîner quatre synchro transmetteurs de couple à puissance élevée de grandeur onze, un synchro différentiel et deux résolvers, pouvant tous être excités séparément. Chaque synchro transmetteur de couple est capable d'entraîner jusqu'à quatre synchro récepteurs à couple élevé.  1, record 10, French, - synchro%20r%C3%A9cepteur%20%C3%A0%20couple%20%C3%A9lev%C3%A9

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, 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 11, English, - gyroscopic%20heading%20and%20attitude%20reference%20system

Record 11,  Textual support,  French

Record number: 11, 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 11, French, - centrale%20gyroscopique%20de%20cap%20et%20de%20verticale

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 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 13, English, - dual%20INS%20configuration

Record 13,  Textual support,  French

Record number: 13, 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 13, French, - configuration%20navigation%20inertielle%20%C3%A0%20double%20redondance

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 CONT

The electronic flight instruments(EFI) consist of three(L, C, R) symbol generators(SG), and two control panels(CP), two Attitude Director Indicators(ADI), and two Horizontal Situation Indicators(HSI). These instruments depend on the Flight Management Computer for flight progress and map background data, the Inertial Reference System for attitude and heading data and the symbol generator.  3, record 14, English, - electronic%20flight%20instruments

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 OBS

Terme et abréviation uniformisés par le CUTA opérations aériennes.  2, record 14, French, - instruments%20%C3%A9lectroniques%20de%20vol

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, 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 15, English, - jerky%20engagement

Record 15,  Textual support,  French

Record number: 15, 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 15, French, - r%C3%A9actions%20brusques%20%C3%A0%20l%27engagement

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 CONT

Ferranti is in the navigation computer field with the autoplan/PODS which allows military crews to insert digitized flight plan data rapidly into an airborne navigation system before take-off. Sea Harrier has the Ferranti NAVHARS navigation heading and attitude reference system.  1, record 16, English, - navigation%20heading%20and%20attitude%20reference%20system

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 CONT

Dans le domaine des calculateurs de navigation pour aéronefs militaires, Ferranti a mis au point l'Autoplan/PODS, lequel permet au pilote d'introduire rapidement des données de plan de vol dans le système de navigation avant le décollage. Enfin, la firme produit la centrale de cap et de verticale NAVHARS pour le Sea Harrier.  1, record 16, French, - centrale%20de%20cap%20et%20de%20verticale%20NAVHARS

Record 16,  Textual support,  Spanish