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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

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

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

Product Details:
Place of Origin: China
Brand Name: NAVI OPTICS
Certification: CCS
Model Number: DINS-100
Document: DINS-100.pdf
Payment & Shipping Terms:
Minimum Order Quantity: one set
Packaging Details: Carton box
Payment Terms: T/T

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

Description
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

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


Contact Details
QINGDAO THUNDSEA MARINE TECHNOLOGY CO.,LTD

Contact Person: Yu.Jing

Tel: +8613045000776

Fax: 86-532-68977475

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