TERMIUM Plus^®

Fiche 1,  Justifications,  Anglais

Record number: 1, Textual support number: 1 CONT

Commerce Control List-Numerical Indexes... "Source code" for the "use" of any inertial navigation equipment or Attitude and Heading Reference Systems(AHRS)(except gimbaled AHRS) including inertial equipment not controlled by 7A003 or 7A004.  1, fiche 1, Anglais, - gimbaled%20AHRS

Record number: 1, Textual support number: 1 OBS

gimballed.  3, fiche 1, Anglais, - gimbaled%20AHRS

Record number: 1, Textual support number: 2 OBS

gimbaled  4, fiche 1, Anglais, - gimbaled%20AHRS

Fiche 1,  Justifications,  Français

Record number: 1, 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.  1, fiche 1, Français, - centrale%20d%27attitude%20et%20de%20cap%20%C3%A0%20cardans

Fiche 1,  Justifications,  Espagnol

Fiche 2,  Justifications,  Anglais

Record number: 2, 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, fiche 2, Anglais, - dual%20redundant%20inertial%20navigation%20system

Fiche 2,  Justifications,  Français

Record number: 2, 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, fiche 2, Français, - syst%C3%A8me%20de%20navigation%20inertielle%20%C3%A0%20double%20redondance

Fiche 2,  Justifications,  Espagnol

Fiche 3,  Justifications,  Anglais

Record number: 3, 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, fiche 3, Anglais, - triple%20redundant%20inertial%20navigation%20system

Fiche 3,  Justifications,  Français

Record number: 3, 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, fiche 3, Français, - syst%C3%A8me%20de%20navigation%20inertielle%20%C3%A0%20triple%20redondance

Fiche 3,  Justifications,  Espagnol

Fiche 4,  Justifications,  Anglais

Record number: 4, 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, fiche 4, Anglais, - dual%20INS%20configuration

Fiche 4,  Justifications,  Français

Record number: 4, 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, fiche 4, Français, - configuration%20navigation%20inertielle%20%C3%A0%20double%20redondance

Fiche 4,  Justifications,  Espagnol

Fiche 5,  Justifications,  Anglais

Record number: 5, Textual support number: 1 CONT

Two clutched heading reference sources are available (one from each inertial navigation set); however, the AFCS obtains heading data from only one of the two sources at any time.  1, fiche 5, Anglais, - clutched%20heading%20reference%20source

Fiche 5,  Justifications,  Français

Fiche 5,  Justifications,  Espagnol

Fiche 6,  Justifications,  Anglais

Record number: 6, Textual support number: 1 CONT

The NAV SOURCE INS-1/INS-2 switchlight is used by the NAVCOM to select INS-1 or INS-2 as a source of heading on the NAVCOM HSI (horizontal situation indicator) compass card.  1, fiche 6, Anglais, - heading%20source

Fiche 6,  Justifications,  Français

Record number: 6, 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, fiche 6, Français, - source%20de%20cap

Fiche 6,  Justifications,  Espagnol