TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

Three Axis Magnetometer [-] TAM... Redundant TAMs are provided to sense the local strength and direction of the Earth's magnetic field. Each TAM consists of a sensor and a separately packaged electronics unit. The analog outputs provided by the TAM allow for sensing magnetic field data in three orthogonal axes. TAM-Operation Once the TAM is powered there will be no ground interactions necessary. The TAM data is used by the FSW ACS [Flight Software Attitude Control Subsystem routine to determine the local magnetic field when reaction wheel momentum unloading is deemed necessary via the magnetic torque rods [Landsat].  3, record 1, English, - three%20axis%20magnetometer

Record number: 1, Textual support number: 1 OBS

three axis magnetometer; CAM: term and abbreviation officially approved by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 1, English, - three%20axis%20magnetometer

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 CONT

On peut mesurer ainsi l'intensité d'un champ magnétique axial. Certains magnétomètres plus sophistiqués peuvent mesurer un champ global selon ses 3 axes x, y et z. On parle alors de magnétomètre triaxial.  2, record 1, French, - magn%C3%A9tom%C3%A8tre%20triaxial

Record number: 1, Textual support number: 1 OBS

magnétomètre triaxial : terme uniformisé par le Groupe de travail de la terminologie de Radarsat-2 (GTTR0).  3, record 1, French, - magn%C3%A9tom%C3%A8tre%20triaxial

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

Attitude control sensors and actuators are monitored by a common electronic unit(the Attitude Sensor Electronics, or ASE), in charge in particular of attitude anomaly detection, and safe mode implementation.  2, record 2, English, - attitude%20sensor%20electronics

Record 2,  Textual support,  French

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

A small, specially-marked satellite, the Canadian Target Assembly(CTA) was deployed on flight day nine to support SVS [Space Vision System]. Also in cargo bay, the Attitude Sensor Package, featuring three European Space Agency independent sensors mounted on a Hitchhiker plate in cargo bay : Modular Star Sensor, Yaw Earth Sensor and Low Altitude Conical Earth Sensor, and the Tank Pressure Control Experiment/Thermal Phenomena(TPCE/TP), contained in a Get Away Special(GAS) canister.  2, record 3, English, - yaw%20Earth%20sensor

Record 3,  Textual support,  French

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, 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 4, English, - inertial%20reference

Record 4,  Textual support,  French

Record number: 4, 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 4, French, - r%C3%A9f%C3%A9rence%20inertielle

Record number: 4, 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 4, French, - r%C3%A9f%C3%A9rence%20inertielle

Record 4,  Textual support,  Spanish