BASED ON CLOSED‑LOOP FIBER‑OPTIC GYROSCOPES

Moscow

Perm

+7 (495) 481-01-27

Applications & Projects

About

Products

En

Ru

BASED ON RING LASER GYROSCOPES

BASED ON CLOSED‑LOOP FIBER‑OPTIC GYROSCOPES

BASED ON MEMS

INS

Gyrolab develops and serially manufactures a broad range of INS products

Home

Products

>

INS

GL-80.009

Initial heading determination error (σ), max, °	0.4 / cos (φ)
Heading hold error over 1 hour of operation (σ), max, °	0.15
Roll / pitch angle determination error (σ), max, °	0.1
Position dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	1
Altitude dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	0.3
Range: X/Y/Z, °/s	±540
Linear acceleration range: X/Y/Z (g)	±10 (optional up to 30 g)

Learn more →

ГЛ-ВГ80.009

GL-90.008

Initial heading determination error (σ), max, °	0.2 / cos (φ)
Heading hold error over 1 hour of operation (σ), max, °	0.06
Roll / pitch angle determination error (σ), max, °	0.06
Position dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	0.6
Altitude dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	0.3
Range: X/Y/Z, °/s	±400
Linear acceleration range: X/Y/Z (g)	±10 (optional up to 30 g)

Learn more →

ГЛ-ВГ90.008

GL-100.018

Initial heading determination error (σ), max, °	0.12 / cos (φ)
Heading hold error over 1 hour of operation (σ), max, °	0.05
Roll / pitch angle determination error (σ), max, °	0.04
Position dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	0.4
Altitude dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	0.3
Range: X/Y/Z, °/s	±500
Overall dimensions (L x W x H), mm, max with shock mount / without shock mount	207x233x160 / 166x154x155
Weight, kg, max with shock mount / without shock mount	6.2 / 4

Learn more →

ГЛ-ВГ100.018

GL-120.016

Initial heading determination error (σ), max, °	0.08 / cos (φ)
Heading hold error over 1 hour of operation (σ), max, °	0.04
Roll / pitch angle determination error (σ), max, °	0.03
Position dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	0.25
Altitude dead-reckoning error (σ) with correction from an external speed sensor, max, % (of travelled distance)	0.2
Range: X/Y/Z, °/s	±500
Overall dimensions (L x W x H), mm, max with shock mount / without shock mount	274x223x161 / -
Weight, kg, max with shock mount / without shock mount	8.9 / -

Learn more →

ГЛ-ВГ120.016

GL-150

The GL-150 inertial navigation system is designed to determine and output orientation and navigation parameters for moving or stationary objects,
with the option to use data from:

GPS/GLONASS satellite navigation system,
a speed sensor,
an altitude/depth sensor.

The system can be used for marine, aviation, and ground applications.

Initial heading determination error (σ), max, °	0.08 / cos (latitude)
Heading hold error over 1 hour of operation (σ), max, °	0.04
Roll / pitch angle determination error (σ), max, °	0.03
Position dead-reckoning error (σ) with correction from an odometer / air data system (ADS) / speed log, max, % (of travelled distance)	0.25
Altitude dead-reckoning error (σ) with correction from an odometer / air data system (ADS) / speed log, max, % (of travelled distance)	0.2
Range: X/Y/Z, °/s	±500
Linear acceleration range: X/Y/Z (g)	±10 (optional up to 30 g)