TERMIUM Plus^®

Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 CONT

In the case of three-axis stabilization, also known as body stabilization, the stabilization is achieved by controlling the movement of the satellite along the three axes, i. e. yaw, pitch and roll, with respect to a reference... The system uses reaction wheels or momentum wheels to correct orbit perturbations.  2, record 1, English, - three%2Daxis%20stabilization

Record 1,  Textual support,  French

Record number: 1, Textual support number: 1 DEF

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

Record number: 1, Textual support number: 1 OBS

stabilisation sur trois axes; stabilisation trois axes : désignations et définition publiées au Journal officiel de la République française le 31 décembre 2005.  2, record 1, French, - stabilisation%20sur%20trois%20axes

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 CONT

The 737 yaw damper system improves ride comfort by sensing turbulence or airplane-generated yaw … The system is initially activated by the yaw damper switch on the overhead panel in the cockpit and is continuously engaged during normal operations; all inputs are automatic and require no pilot action.  2, record 2, English, - yaw%20damper%20switch

Record 2,  Textual support,  French

Record number: 2, Textual support number: 1 OBS

interrupteur de l'amortisseur de lacet : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) – Opérations aériennes.  2, record 2, French, - interrupteur%20de%20l%27amortisseur%20de%20lacet

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

Some AFCS [automatic flight control system] retain the use of the yaw channel to provide simple heading hold in forward flight while others use turn-coordination in yaw and hold heading by adjusting AOB [angle of bank].  2, record 3, English, - yaw%20channel

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

chaîne de lacet : terme uniformisé par le Comité d'uniformisation de la terminologie aéronautique (CUTA) – Opérations aériennes.  2, record 3, French, - cha%C3%AEne%20de%20lacet

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 DEF

A control system or device that reduces the yaw of an aircraft.  2, record 4, English, - yaw%20damper

Record number: 4, Textual support number: 1 OBS

The term "yaw" may be defined as the angular motion about the vertical axis on the normal axis of an aircraft.  3, record 4, English, - yaw%20damper

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 DEF

Dispositif de stabilisation automatique atténuant les oscillations d'un aéronef autour de son axe vertical (axe de lacet).  2, record 4, French, - amortisseur%20de%20lacet

Record number: 4, Textual support number: 1 OBS

amortisseur de lacet : terme normalisé par le Ministère de la défense de la France.  3, record 4, French, - amortisseur%20de%20lacet

Record number: 4, Textual support number: 2 OBS

amortisseur de lacet : terme uniformisé par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  4, record 4, French, - amortisseur%20de%20lacet

Record 4,  Textual support,  Spanish

Record number: 4, Textual support number: 1 CONT

La función de amortiguador de guiñada asegura [...] en el control automático: el cumplimiento de las órdenes del piloto automático de la gestión de vuelo y orientación.  1, record 4, Spanish, - amortiguador%20de%20gui%C3%B1ada

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 DEF

A horizontal-axis wind turbine [provided with a] yaw control system that uses an electrical or hydraulic servomechanism to orient the rotor with the wind in response to a signal from a wind vane.  4, record 5, English, - active%20yaw%20wind%20turbine

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 DEF

Éolienne à axe horizontal munie d'un dispositif d'orientation utilisant un servomécanisme électrique ou hydraulique pour diriger le rotor vers le vent en réponse à un signal provenant du gouvernail.  2, record 5, French, - %C3%A9olienne%20%C3%A0%20m%C3%A9canisme%20d%27orientation%20actif

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record number: 6, Textual support number: 1 DEF

A yaw system [that] aligns a HAWT [horizontal-axis wind turbine] with the wind.  3, record 6, English, - tail%20vane

Record number: 6, Textual support number: 1 CONT

Most micro and mini systems use a simple tail vane that directs the rotor into the wind. In some systems, the rotor is downwind of the generator, so it naturally aligns with the wind.  3, record 6, English, - tail%20vane

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 DEF

Dispositif d'orientation généralement constitué d'une surface plane située à l'arrière de la tête [d'une] éolienne, à l'extrémité d'une poutre-support, et qui permet de maintenir l'aéromoteur face au vent.  5, record 6, French, - gouvernail

Record number: 6, Textual support number: 1 CONT

Pour les aéromoteurs de petite et moyenne puissance dont l'hélice est placée en avant du pylône, le dispositif d'orientation est un gouvernail généralement constitué par une surface plane (plaque métallique ou en bois) placée à l'extrémité d'une poutre-support solidaire du corps de la machine.  6, record 6, French, - gouvernail

Record 6,  Textual support,  Spanish

Record number: 6, Textual support number: 1 DEF

Pala que, por la acción del viento, orienta las aspas de los aeromotores.  1, record 6, Spanish, - tim%C3%B3n

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 CONT

Due to the allowable rapid yaw rates of wind turbines with blade cyclic pitch variation, the two conventional separate control systems-yaw control for wind direction following and blade feathering control for regulating rotor speed and torque-can be replaced by a system with only a single control variable, the rotor yaw angle.  1, record 7, English, - blade%20feathering%20control

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 OBS

La régulation de puissance par mise en drapeau consiste à obliger les pales à pivoter autour de leur axe mécanique de façon à réduire l’angle d’attaque, donc le C_z et enfin le couple moteur. Cette réduction de l’angle d’attaque est obtenue par augmentation du calage (angle que fait la corde du profil avec le plan de rotation de l’hélice) moyen des pales.  2, record 7, French, - syst%C3%A8me%20de%20r%C3%A9gulation%20de%20puissance%20par%20mise%20en%20drapeau

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 CONT

The upper rudder is electric and receives input from the yaw stability augmentation system. The lower rudder receives input from the Flight Guidance System.  3, record 8, English, - yaw%20stability%20augmentation%20system

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 OBS

On étudie la stabilité d'un aéronef sur trois axes: la stabilité en lacet, capacité de l'aéronef à conserver sa direction [ ;] la stabilité en tangage, capacité de l'aéronef à conserver son assiette [ ;] la stabilité en roulis, capacité de l'aéronef à conserver son inclinaison en ligne droite et en virage.  3, record 8, French, - syst%C3%A8me%20d%27augmentation%20de%20stabilit%C3%A9%20en%20lacet

Record number: 8, Textual support number: 2 OBS

système d'augmentation de stabilité en lacet ; SAS lacet : termes uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes.  3, record 8, French, - syst%C3%A8me%20d%27augmentation%20de%20stabilit%C3%A9%20en%20lacet

Record 8,  Textual support,  Spanish

Record 9,  Textual support,  English

Record number: 9, Textual support number: 1 DEF

A feedback control system that provides pitch, roll, or yaw damping; sometimes called a "damper. "  3, record 9, English, - stability%20augmentation%20system

Record number: 9, Textual support number: 1 OBS

Older aircraft with an SAS use an electrical, single-loop feedback signal in parallel (stick moves) or series (stick doesn’t move) with the mechanical flight control system.  3, record 9, English, - stability%20augmentation%20system

Record number: 9, Textual support number: 1 PHR

Automatic stability augmentation system.  4, record 9, English, - stability%20augmentation%20system

Record 9,  Textual support,  French

Record number: 9, Textual support number: 1 OBS

système d'augmentation de stabilité; SAS : terme et abréviation uniformisés par les Comités d'uniformisation de la terminologie aéronautique (CUTA) - Opérations aériennes et Maintenance.  3, record 9, French, - syst%C3%A8me%20d%27augmentation%20de%20stabilit%C3%A9

Record 9,  Textual support,  Spanish

Record 10,  Textual support,  English

Record number: 10, Textual support number: 1 CONT

The Cessna 750 has a yaw control system provided by a lower rudder and an upper rudder. Each rudder surface has an independent full-time control system, except that they share mechanical input at the rudder pedals. The lower surface is controlled by mechanical input to hydraulically-powered actuators. The upper surface is electronically controlled. The lower rudder is positioned by two identical power control units(PCUs) installed one above the other, in parallel, in the vertical fin.  2, record 10, English, - lower%20rudder

Record 10,  Textual support,  French

Record number: 10, Textual support number: 1 OBS

gouvernail inférieur de direction; gouverne inférieure de direction : termes uniformisés par le Comité d'uniformisation de la terminologie aéronautique (CUTA) - Maintenance.  2, record 10, French, - gouvernail%20inf%C3%A9rieur%20de%20direction

Record 10,  Textual support,  Spanish

Record 11,  Textual support,  English

Record number: 11, Textual support number: 1 CONT

Each SRB [solid rocket booster] contains two RGAs [rate gyro assembly], with each RGA containing one pitch and one yaw gyro. These provide an output proportional to angular rates about the pitch and yaw axes to the orbiter computers and guidance, navigation and control system during first-stage ascent flight in conjunction with the orbiter roll rate gyros until SRB separation.  3, record 11, English, - yaw%20gyroscope

Record 11,  Textual support,  French

Record number: 11, Textual support number: 1 CONT

Les premiers vols se sont avérés critiques surtout que nous n'avions qu'un gyro en tangage, pas de barre de Bell et une tête rigide. [...] pour le confort de pilotage, un gyro de lacet s'est vite avéré indispensable.  2, record 11, French, - gyroscope%20de%20lacet

Record 11,  Textual support,  Spanish

Record 12,  Textual support,  English

Record number: 12, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : Vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, record 12, English, - roll%20axis

Record number: 12, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation: roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle’s centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight. ... The axes of a cylindrical spacecraft (e.g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft (i.e. defined relative to the pilot’s seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc": the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth’s spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  4, record 12, English, - roll%20axis

Record number: 12, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  4, record 12, English, - roll%20axis

Record number: 12, Textual support number: 2 OBS

roll axis; axis of roll: terms officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  5, record 12, English, - roll%20axis

Record 12,  Textual support,  French

Record number: 12, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  1, record 12, French, - axe%20de%20roulis

Record number: 12, Textual support number: 1 OBS

axe de roulis : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  2, record 12, French, - axe%20de%20roulis

Record 12,  Textual support,  Spanish

Record 13,  Textual support,  English

Record number: 13, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : Vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by Vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  2, record 13, English, - pitch%20axis

Record number: 13, Textual support number: 2 CONT

Spacecraft axes. The three orthogonal axes of rotation: roll, pitch and yaw. If the spacecraft has a recognisable longitudinal axis or a specified forward direction of flight, the axes are analogous to those of an aircraft, where the roll axis is the longitudinal axis; the pitch axis is in the plane of the wings; and the yaw axis is the "vertical" axis, orthogonal to both the roll and pitch axes. The axes are mutually perpendicular, with an "origin" at the vehicle’s centre of mass. For a winged spacecraft such as a Space Shuttle, the similarity with an aircraft is obvious. For expendable launch vehicles the roll axis is the axis which is vertical at launch and the other axes are more-or-less arbitrarily assigned since the vehicle rotates about the roll axis in flight. ... The axes of a cylindrical spacecraft (e.g. Apollo, Suyuz, etc.) are similar to those of an ELV [Expendable Launch Vehicle] at launch, but one orbit assume the axis-definition of an aircraft (i.e. defined relative to the pilot’s seat). The axes of a satellite mirror those of an aircraft "flying along the orbital arc": the roll axis is aligned with the direction of travel; the yaw axis passes through the sub-satellite point; and the pitch axis is orthogonal to the other two. For a satellite in an equatorial orbit, the pitch axis is aligned approximately with the Earth’s spin axis. The pitch axis is also the spin axis for the spin-stabilised satellite.  3, record 13, English, - pitch%20axis

Record number: 13, Textual support number: 1 OBS

In the compilation of engineering drawings the three orthogonal axes are often labelled in Cartesian fashion: x=roll, y=pitch, z=yaw. For the three-axis stabilised spacecraft, the x-axis and y-axis are otherwise known as the east-west and north-south axes, respectively; the z-axis passes through the sub-satellite point. This leads to the definition of the box-shaped satellite’s faces as follows: the "plus-x face" faces east; the "minus-x face" faces west; +y faces south; -y faces north; +z is the Earth-pointing face; and -z is the "anti-Earth face."  3, record 13, English, - pitch%20axis

Record number: 13, Textual support number: 2 OBS

pitch axis: term officially approved by the International Space Station official approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 13, English, - pitch%20axis

Record 13,  Textual support,  French

Record number: 13, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  2, record 13, French, - axe%20de%20tangage

Record number: 13, Textual support number: 1 OBS

axe de tangage : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2.  3, record 13, French, - axe%20de%20tangage

Record 13,  Textual support,  Spanish

Record 14,  Textual support,  English

Record number: 14, Textual support number: 1 DEF

The rotation of a vehicle about its vertical (Z) axis, i.e. movement in azimuth.  2, record 14, English, - yaw

Record number: 14, Textual support number: 1 CONT

The local orbital reference system is defined at each point of the orbit by three unit vectors. These vectors are derived from the satellite position and velocity vectors : vector L is colinear with position vector P(on the axis between the Earth's centre and the satellite). It defines the yaw axis. Vector T is perpendicular to the orbital plane(vector L, vector V). It defines the pitch axis. Vector R completes the set of orthogonal axes. It lies in the plane defined by vectors L and V and defines the roll axis. It does not coincide exactly with the velocity vector due to the eccentricity of the orbit.  3, record 14, English, - yaw

Record number: 14, Textual support number: 1 OBS

yaw: term officially approved by the International Space Station Official Approval Group (ISSOAG) and by the RADARSAT-2 Terminology Approval Group (RTAG).  4, record 14, English, - yaw

Record 14,  Textual support,  French

Record number: 14, Textual support number: 1 DEF

Mouvement d'un corps autour d'un axe perpendiculaire aux axes de roulis et de tangage.  2, record 14, French, - lacet

Record number: 14, Textual support number: 1 CONT

Le repère orbital local est défini en chaque point de l'orbite par les trois vecteurs unitaires. Ces vecteurs sont construits à partir du vecteur position et du vecteur vitesse du satellite : Le vecteur L est colinéaire au vecteur position P (sur l'axe centre Terre, satellite). Il définit l'axe de lacet. Le vecteur T est perpendiculaire au plan de l'orbite (vecteur L, vecteur V). Il définit l'axe de tangage. Le vecteur R complète le trièdre. Il appartient au plan (vecteur L, vecteur V) et définit l'axe de roulis. Il ne coïncide pas exactement avec le vecteur vitesse à cause de l'excentricité de l'orbite.  3, record 14, French, - lacet

Record number: 14, Textual support number: 1 OBS

lacet : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI) et par le Groupe de travail de la terminologie de RADARSAT-2 (GTTR).  4, record 14, French, - lacet

Record 14,  Textual support,  Spanish

Record 15,  Textual support,  English

Record number: 15, Textual support number: 1 DEF

A horizontal-axis wind turbine yaw control system that uses the natural aerodynamic forces of the wind to orient the nacelle and rotor in proper alignment with the wind.  2, record 15, English, - passive%20yaw%20control

Record 15,  Textual support,  French

Record number: 15, Textual support number: 1 DEF

Système de contrôle du lacet d'une éolienne à axe horizontal qui fait appel aux forces aérodynamiques naturelles du vent pour aligner correctement la nacelle et le rotor vers le vent.  2, record 15, French, - orientation%20passive

Record 15,  Textual support,  Spanish

Record 16,  Textual support,  English

Record number: 16, Textual support number: 1 DEF

A horizontal-axis wind turbine yaw control system that uses an electrical or hydraulic servomechanism to orient the rotor with the wind in response to a signal from a wind vane.  2, record 16, English, - active%20yaw%20control

Record 16,  Textual support,  French

Record number: 16, Textual support number: 1 DEF

Système d'orientation d'une éolienne à axe horizontal utilisant un servomécanisme électrique ou hydraulique pour diriger le rotor vers le vent en réponse à un signal provenant du gouvernail.  2, record 16, French, - orientation%20active

Record 16,  Textual support,  Spanish

Record 17,  Textual support,  English

Record number: 17, Textual support number: 1 DEF

Numerical calculations used to measure wind velocity and direction that are transmitted to a wind turbine yaw drive system to orient the turbine properly with respect to the wind.  2, record 17, English, - wind%20values

Record number: 17, Textual support number: 1 OBS

Wind velocity values are generally expressed in kilometers/second.  2, record 17, English, - wind%20values

Record number: 17, Textual support number: 2 OBS

The strength of a downdraft varies with the obstruction and the wind value. Higher wind values produce more turbulence and stronger downdrafts.  2, record 17, English, - wind%20values

Record 17,  Textual support,  French

Record number: 17, Textual support number: 1 DEF

Calculs numériques utilisés pour déterminer la vélocité et la direction du vent que l'on transmet au système d'orientation d'une éolienne afin de positionner correctement cette dernière en fonction du vent.  2, record 17, French, - valeurs%20%C3%A9oliennes

Record number: 17, Textual support number: 1 OBS

Les valeurs éoliennes portant sur la vitesse du vent sont généralement exprimées en kilomètres/seconde.  2, record 17, French, - valeurs%20%C3%A9oliennes

Record 17,  Textual support,  Spanish

Record 18,  Textual support,  English

Record number: 18, Textual support number: 1 CONT

The carrier is fitted with the SATRAP computerised, integrated stabilisation system designed to maintain stabilisation to within 0. 5º of horizontal, allowing aircraft to be operated up to Sea State 5/6. As well as the carrier's two pairs of active stabilising fins and twin rudders, the system has two computer-controlled compensation units which consist of two rail tracks for trains carrying 22t of deadweight. These tracks run transversely below the flight deck. The system is designed to compensate for wind and heel and control roll, yaw and surge.  1, record 18, English, - SATRAP

Record 18,  Textual support,  French

Record number: 18, Textual support number: 1 CONT

[...] SATRAP, un système automatique de tranquillisation et de pilotage qui permet de réduire les mouvements de roulis, de lacet et d'embardée du porte-avions et comprend notamment un dispositif révolutionnaire de compensation de gîte consistant en douze trains de wagonnets lestés se déplaçant sous le pont d'envol.  1, record 18, French, - SATRAP

Record 18,  Textual support,  Spanish

Record 19,  Textual support,  English

Record number: 19, 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 19, English, - ISS%20attitude

Record number: 19, Textual support number: 1 OBS

ISS attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 19, English, - ISS%20attitude

Record 19,  Textual support,  French

Record number: 19, 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 19, French, - attitude%20de%20la%20Station%20spatiale

Record 19,  Textual support,  Spanish

Record 20,  Textual support,  English

Record number: 20, 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 20, English, - local%20vertical%20local%20horizontal

Record number: 20, 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 20, English, - local%20vertical%20local%20horizontal

Record number: 20, 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 20, English, - local%20vertical%20local%20horizontal

Record 20,  Textual support,  French

Record number: 20, 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 20, French, - local%20vertical%20local%20horizontal

Record 20,  Textual support,  Spanish

Record 21,  Textual support,  English

Record number: 21, 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 21, English, - yaw%20Earth%20sensor

Record 21,  Textual support,  French

Record 21,  Textual support,  Spanish

Record 22,  Textual support,  English

Record number: 22, Textual support number: 1 CONT

... CEVIS is used for systemic aerobic conditioning and can be applied to independent upper and lower limb activity. As with the TVIS, its vibration isolation system counteracts(isolates) translations in x, y, and z, as well as roll, pitch and yaw.  3, record 22, English, - cycle%20ergometer%20with%20vibration%20isolation%20system

Record number: 22, Textual support number: 1 OBS

cycle ergometer with vibration isolation system; CEVIS: term and abbreviation officially approved by the International Space Station official approval Group (ISSOAG).  4, record 22, English, - cycle%20ergometer%20with%20vibration%20isolation%20system

Record 22,  Textual support,  French

Record number: 22, Textual support number: 1 CONT

Le nouvel ergocycle CEVIS (Cycle Ergometer with Vibration Isolation System) a été mis en place au cours de la semaine, tandis que les ingénieurs se sont penchés sur les corrections à apporter au tapis roulant de la station. Les plaques de support de l'appareil destiné à éliminer le plus possible les vibrations parasites pour les expériences réalisées lors de séances d'exercice présentent des signes d'usure.  2, record 22, French, - ergocycle%20CEVIS

Record number: 22, Textual support number: 1 OBS

ergocycle CEVIS : terme uniformisé par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  3, record 22, French, - ergocycle%20CEVIS

Record 22,  Textual support,  Spanish

Record 23,  Textual support,  English

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

Record 23,  Textual support,  French

Record number: 23, 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 23, French, - r%C3%A9f%C3%A9rence%20inertielle

Record number: 23, 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 23, French, - r%C3%A9f%C3%A9rence%20inertielle

Record 23,  Textual support,  Spanish

Record 24,  Textual support,  English

Record number: 24, Textual support number: 1 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.  2, record 24, English, - pitch%20pickoff

Record number: 24, Textual support number: 2 CONT

The AUTOFLUG FGC T is a cold-gas driven free displacement gyroscope concerning roll axis and yaw(pitch) axis. The FGC T consists of the following subassemblies : Gyroscope housing, gimbal bolt mechanism, gimbal system. Gyroscope drive consisting of : gas bottle and locking mechanism, roll pickoff, pitch pickoff and pickoff electronic.  3, record 24, English, - pitch%20pickoff

Record 24,  Textual support,  French

Record number: 24, Textual support number: 1 CONT

Les capteurs mesurant des angles autour d'axes proches de l'axe X du satellite sont généralement qualifiés de capteurs de roulis, les capteurs mesurant des angles autour d'axes proches de l'axe Y sont de même qualifiés de capteurs de tangage, et les capteurs mesurant des angles autour d'axes proches de l'axe Z sont qualifiés de capteurs de lacet. Ceci ne signifie pas que ces capteurs mesurent des angles de Cardan à partir d'un repère de référence inertiel, ils peuvent très bien mesurer par exemple un angle dièdre entre le plan (X, Z) et le plan (X, Soleil), on parlera dans ce cas d'un capteur de roulis Soleil.  2, record 24, French, - capteur%20de%20tangage

Record number: 24, Textual support number: 2 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.  3, record 24, French, - capteur%20de%20tangage

Record number: 24, Textual support number: 1 OBS

Quand le véhicule est connecté à un PC par un lien, l'interface permet d'agir directement sur les actionneurs (propulseur et gouvernes). Cette interface permet aussi de visualiser en temps réel, les données issues des capteurs : roulis, tangage, lacet, profondeur, vitesse de roulis et de tangage, ainsi que d'afficher les coordonnées fournies par le récepteur GPS.  4, record 24, French, - capteur%20de%20tangage

Record 24,  Textual support,  Spanish

Record 25,  Textual support,  English

Record number: 25, 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 25, English, - Station%27s%20flight%20attitude

Record number: 25, Textual support number: 1 OBS

Station’s flight attitude: term officially approved by the International Space Station official approval Group (ISSOAG).  3, record 25, English, - Station%27s%20flight%20attitude

Record 25,  Textual support,  French

Record number: 25, 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 25, French, - attitude%20de%20la%20Station

Record number: 25, 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 25, French, - attitude%20de%20la%20Station

Record 25,  Textual support,  Spanish

Record 26,  Textual support,  English

Record number: 26, Textual support number: 1 DEF

The pre-arranged meeting (and usu. docking) of two or more spacecraft in space.  2, record 26, English, - rendezvous

Record number: 26, Textual support number: 1 CONT

The final phase of rendezvous operations begins about three hours prior to Atlantis’ docking with the ISS [International Space Station]. Atlantis will approach the ISS from below, in what is referred to as a plus-R bar approach, to minimize the effects of jet thruster firings on the station and its solar arrays. About 40 minutes before the terminal initiation burn(Ti burn) when Atlantis moves within 135, 000 feet of the station, the shuttle's rendezvous radar system is activated to provide supplemental navigation information. Prior to initiating the Ti burn, the crew will power on the ODS [Orbital Docking System] and activate Atlantis's docking lights. A series of course correction burns will bring Atlantis to a point almost directly below and behind the station, at which point Commander Ken Cockrell initiates the manual portion of his approach to the ISS. Atlantis will intercept the R-bar about 700 feet below the station. Cockrell will slowly move Atlantis to a point about 600 feet below the station before performing a 180 degree yaw maneuver to position Atlantis in a "tail forward" attitude for the final approach and docking.  3, record 26, English, - rendezvous

Record number: 26, Textual support number: 1 OBS

rendezvous: term officially approved by the International Space Station official approval Group (ISSOAG).  4, record 26, English, - rendezvous

Record number: 26, Textual support number: 1 PHR

Rendezvous burn, flight.  4, record 26, English, - rendezvous

Record number: 26, Textual support number: 2 PHR

Phase of rendezvous.  4, record 26, English, - rendezvous

Record 26,  Textual support,  French

Record number: 26, Textual support number: 1 DEF

Opération par laquelle un véhicule spatial en rejoint un autre en orbite autour de la Terre ou d'un autre corps céleste.  4, record 26, French, - rendez%2Dvous

Record number: 26, Textual support number: 1 OBS

rendez-vous; rendez-vous spatial : termes uniformisés par le Groupe de travail de la terminologie de la Station spatiale internationale (GTTSSI).  5, record 26, French, - rendez%2Dvous

Record number: 26, Textual support number: 1 PHR

Rendez-vous entièrement automatique.  6, record 26, French, - rendez%2Dvous

Record 26,  Textual support,  Spanish

Record 27,  Textual support,  English

Record number: 27, Textual support number: 1 CONT

The current air data system comprises fuselage-mounted probes, which are intended to gather three types of information-static and dynamic pressure, temperatures and airstream direction indicating angle of attack and yaw.  1, record 27, English, - airstream%20direction

Record 27,  Textual support,  French

Record 27,  Textual support,  Spanish

Record 28,  Textual support,  English

Record number: 28, Textual support number: 1 OBS

The Yaw channel amplification system consists of the following components contained in the Amplifier.(...)-One Yaw washout network with a yaw washout amplifier(...)  1, record 28, English, - Yaw%20washout%20amplifier

Record number: 28, Textual support number: 2 OBS

The complete source code is MECAR-SE-210E,1970,1,22-11-0,1  2, record 28, English, - Yaw%20washout%20amplifier

Record 28,  Textual support,  French

Record 28,  Textual support,  Spanish

Record 29,  Textual support,  English

Record number: 29, Textual support number: 1 OBS

The Yaw channel amplification system consists of the following components contained in the Amplifier.(...)-One Yaw washout network with a yaw washout amplifier(...)  1, record 29, English, - Yaw%20washout%20network

Record number: 29, Textual support number: 2 OBS

The complete source code is MECAR-SE-210E,1970,1,22-11-0,1  2, record 29, English, - Yaw%20washout%20network

Record 29,  Textual support,  French

Record 29,  Textual support,  Spanish

Record 30,  Textual support,  English

Record number: 30, Textual support number: 1 CONT

As a four-axis system, DFC-500 controls pitch, roll, yaw and collective(vertical flight). It offers pedal-controlled heading selection, automatic deceleration at the end of an approach, and automatic hover coupled to radio height.  1, record 30, English, - pedal%2Dcontrolled%20heading%20selection

Record 30,  Textual support,  French

Record number: 30, Textual support number: 1 CONT

Le DFC-500 commande le tangage, le roulis, le lacet et le pas général (vol vertical). Il permet la sélection de cap par action sur le palonnier, la décélération automatique en fin d'approche et le vol stationnaire en mode automatique, avec couplage au radioaltimètre.  1, record 30, French, - s%C3%A9lection%20de%20cap%20par%20action%20sur%20le%20palonnier

Record 30,  Textual support,  Spanish

Record 31,  Textual support,  English

Record number: 31, Textual support number: 1 OBS

Autopilot. That portion of the system that uses radio/radar beam, directional and vertical gyro, pitot static and manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft.  1, record 31, English, - radio%2Fradar%20beam

Record 31,  Textual support,  French

Record number: 31, Textual support number: 1 OBS

Pilote automatique. Partie du système utilisant le faisceau radio/radar, les gyros directionnel et vertical, les informations du circuit de pression statique et totale et les informations introduites manuellement pour commander automatiquement l'aéronef en lacet, en tangage et en roulis.  1, record 31, French, - faisceau%20radio%2Fradar

Record 31,  Textual support,  Spanish