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Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System

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Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System

Brand Name : NAVI OPTICS

Model Number : DINS-100

Certification : CCS

Place of Origin : China

MOQ : one set

Payment Terms : T/T

Packaging Details : Carton box

Settling time : 6h

Position : 2nm/10d, peak

Velocity : 0.5m/s, 1σ

Attitude : 0.005deg, 1σ

Heading : 0.008×sec(Lat) deg, 1σ

Heave : 5cm or 5%

Working Temperature : -40℃~+55℃

Storage Temperature : -55℃~+70℃

Dimensions (W x D x H) : φ550×500 mm

Weight : ≤60kg

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Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System


Introduction

DINS 100 dual-axis rotary laser gyro inertial navigation system is a high-performance inertial navigation and measurement equipment, which adopts 90-type two-frequency machine shaking laser gyroscope and quartz flexure accelerometer, and the performance of the system has been significantly improved through high-precision error calibration, temperature compensation technology, and dual-axis rotary on-line autonomous calibration and error self-compensation technology. The system adopts electromagnetic shielding design, thermal balance design, vibration modal design, sealing design and strict manufacturing process to ensure excellent environmental adaptability.


Features

High precision 90 type 2-frequency machine shake laser gyroscope

Dual-axis rotational self-calibration and error self-compensation

Static base and moving base initial alignment

Error parameter calibration and compensation in full temperature range

Preset GNSS/odometer/trip-meter interface

Can be configured to different navigation modes

Excellent environmental adaptability

Military standard


Application

Ship navigation

Underwater submarine navigation

Positioning and Orientation of Missile Launch Vehicles

High-precision Attitude Measurement



Performance
Start-up time 6h
Pure Inertial Position 2nm/10d, peak
Pure Inertial Velocity 0.5m/s, 1σ
Pure Inertial Attitude 0.005deg, 1σ
Pure Inertial Heading 0.008×sec(Lat) deg, 1σ
Heave 5cm or 5%
Measuring Range
Angular Velocity ±400deg/s
Acceleration ±20g
Working Environment
Working Temperature -40℃~+55℃
Storage Temperature -55℃~+70℃
Vibration 0.04g2/hz@ 20~2000hz
Normal Operation/ 30g @ 6ms/50g @ 11 ms

no damage under shock
Electrical Characteristics
Operating Voltage 28VDC
Power Consumption ≤200W
Communication Interface RS422/RS232/CAN/Ethernet
Physical Characteristics
Dimensions (W x D x H) φ550×500 mm
Weight ≤60kg



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Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System Images

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