TERMIUM Plus®

The Government of Canada’s terminology and linguistic data bank.

IMU [9 records]

Record 1 2010-12-02

English

Subject field(s)
  • Flight Instruments and Equipment (Aeroindustry)
  • Aircraft Piloting and Navigation
  • Navigation Instruments
CONT

The gyros are used to maintain the platform's inertial orientation by sensing rotations of the platform caused by vehicle-rotation-induced friction at the gimbal pivot points... One gyro-called the vertical gyro-is oriented so its input axes are aligned with the X and Y platform axes; its input axes provide IMU [Inertial Measurement Unit] platform roll and pitch stabilization. The second gyro is oriented so that one input axis lies along the platform's Z axis and the other lies in the X-Y plane. This gyro-the azimuth gyro-provides platform yaw stabilization with the Z input axis, while the second input axis is used as a platform rate detector for built-in test equipment.

CONT

The sensors for angular velocity are vibrating gyroscopes (3 axes, to detect rotation and pitch/roll pendulations of the payload). An error signal is obtained differencing the signal from the azimuth gyroscope and a constant level settable from the telemetry, which controls the speed of rotation. Such error signal drives an analog PID [Proportional Integral Differential] circuit; the output of the PID is connected to the PWM [Pulse Width Modulation] driver supplying current to the pivot azimuth motors.

CONT

azimuth gyro: term used at Natural Resources Canada - Earth Sciences Sector.

PHR

Azimuth gyro drift rate.

French

Domaine(s)
  • Instruments et équipement de bord (Constructions aéronautiques)
  • Pilotage et navigation aérienne
  • Instruments de navigation
CONT

La plate-forme stabilisée [...] Trois gyroscopes sont utilisés : (a) Un gyroscope d'azimut qui, n'ayant aucun degré de liberté dans l'axe vertical, détecte tout déplacement de la plate-forme en azimut. (b) Deux gyroscopes d'inclinaison [...]

OBS

gyroscope d'azimut : terme en usage à Ressources naturelles Canada - Secteur des sciences de la Terre.

PHR

Vitesse de dérive du gyroscope d'azimut.

Spanish

Save record 1

Record 2 2008-12-23

English

Subject field(s)
  • Flight Instruments and Equipment (Aeroindustry)
  • Spacecraft
CONT

IMU(Inertial Measurement Unit) Test. A common method to align the vehicle's IMU to "the world" is by measuring the local gravity vector with the IMU's accelerometers and comparing it to the theoretical local gravity vector. The angle between the 2 vectors is the vehicle's tilt angle.

French

Domaine(s)
  • Instruments et équipement de bord (Constructions aéronautiques)
  • Engins spatiaux

Spanish

Save record 2

Record 3 2003-10-21

English

Subject field(s)
  • International Bodies and Committees
  • Mathematics
OBS

IMU is an international non-governmental and non-profit scientific organization, with the purpose of promoting international cooperation in mathematics.

French

Domaine(s)
  • Organismes et comités internationaux
  • Mathématiques

Spanish

Campo(s) temático(s)
  • Organismos y comités internacionales
  • Matemáticas
Key term(s)
  • Unión Internacional Matemáticas
Save record 3

Record 4 2001-10-17

English

Subject field(s)
  • Flight Instruments and Equipment (Aeroindustry)
  • Aircraft Piloting and Navigation
  • Navigation Instruments
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.

Key term(s)
  • dual redundant INS

French

Domaine(s)
  • Instruments et équipement de bord (Constructions aéronautiques)
  • Pilotage et navigation aérienne
  • Instruments de navigation
OBS

Le Grippen dispose d'un système de commande de vol électrique digitale à triple redondance et d'une centrale inertielle Honeywell.

Spanish

Save record 4

Record 5 2001-10-17

English

Subject field(s)
  • Flight Instruments and Equipment (Aeroindustry)
  • Aircraft Piloting and Navigation
  • Navigation Instruments
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.

French

Domaine(s)
  • Instruments et équipement de bord (Constructions aéronautiques)
  • Pilotage et navigation aérienne
  • Instruments de navigation
OBS

Le Grippen dispose d'un système de commande de vol électrique digitale à triple redondance et d'une centrale inertielle Honeywell.

Spanish

Save record 5

Record 6 2001-09-14

English

Subject field(s)
  • Flight Instruments and Equipment (Aeroindustry)
  • Aircraft Piloting and Navigation
  • Navigation Instruments
DEF

An inertial guidance system that makes use of a three-gimbal mounting whose inner gimbal is a stable platform on which three gyroscopes and accelerometers are mounted; the gyroscopes sense any rotation of the vehicle and drive the gimbals in the opposite direction, so that the inner platform remains fixed in inertial space.

CONT

Automatic Calibration of Transducers for Gimballed Inertial Navigation System on Uncontrolled Gyros. In the work a new approach to calibration of gimbaled Inertial Navigation system(INS) based on two electrostatically suspended gyros(ESG) is considered. The automatic calibration procedure of the inertial measuring unit(IMU) error models parameters, namely, the gimbal pick-off errors, is examined. The measurement errors for angle rotor position are described by equation. The gimbal pick-off errors are described by equation. The relationship between the gimbal pick-off errors and INS output errors is described by equation.

OBS

Gimballed.

OBS

Gimbaled.

Key term(s)
  • gimballed inertial system

French

Domaine(s)
  • Instruments et équipement de bord (Constructions aéronautiques)
  • Pilotage et navigation aérienne
  • Instruments de navigation
CONT

Un nouveau type de centrale inertielle, déjà utilisée sur des avions comme les Airbus A 310 et A 320 [...] vient concurrencer les centrales inertielles à cardans (gimbaled inertial system). Il s'agit d'une centrale dite à composants liés (sous-entendu à la structure de l'avion) appelée en anglais «strap down inertial system». Dans ce cas, en effet, les accéléromètres et les gyromètres (ou les gyroscopes) sont fixés rigidement sur la structure.

Key term(s)
  • centrale inertielle gyrostabilisée

Spanish

Save record 6

Record 7 2001-06-21

English

Subject field(s)
  • Flight Instruments and Equipment (Aeroindustry)
  • Aircraft Piloting and Navigation
  • Navigation Instruments
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.

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.

French

Domaine(s)
  • Instruments et équipement de bord (Constructions aéronautiques)
  • Pilotage et navigation aérienne
  • Instruments de navigation
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 [...]

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.

OBS

calculateur de navigation : terme d'usage obligatoire au Bureau de la traduction.

Spanish

Save record 7

Record 8 2001-06-21

English

Subject field(s)
  • Flight Instruments and Equipment (Aeroindustry)
  • Aircraft Piloting and Navigation
  • Navigation Instruments
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.

French

Domaine(s)
  • Instruments et équipement de bord (Constructions aéronautiques)
  • Pilotage et navigation aérienne
  • Instruments de navigation
OBS

Le Grippen dispose d'un système de commande de vol électrique digitale à triple redondance et d'une centrale inertielle Honeywell.

Spanish

Save record 8

Record 9 2001-06-21

English

Subject field(s)
  • General Mechanics (Physics)
  • Aircraft Piloting and Navigation
DEF

A coordinate system in which a body moves with constant velocity as long as no force is acting on it.

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.

French

Domaine(s)
  • Mécanique générale (Physique)
  • Pilotage et navigation aérienne

Spanish

Save record 9

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