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Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System with Military Standard
Key Attributes
Brand Name:
NAVI OPTICS
Model Number:
DINS-100
Place of Origin:
China
Certification:
CCS
Minimum Order Quantity:
one set
Payment Terms:
T/T
Standard Packaging:
Carton box
Product Summary
Model DINS-100: High-precision dual-axis rotary laser gyro INS with 2nm/10d positioning accuracy, 0.005° attitude precision, and military-grade durability. Features autonomous calibration, full-temperature compensation, and excellent environmental adaptability for marine and missile applications.
Product Custom Attributes
Highlight
dual-axis rotary laser gyro
,high precision inertial navigation system
,laser gyro navigation system with warranty
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
Product Description
Model DINS-100 High Precision Dual-Axis Rotary Laser Gyro Inertial Navigation System
DINS 100 dual-axis rotary laser gyro inertial navigation system is a high-performance inertial navigation and measurement equipment designed for demanding applications requiring exceptional precision and reliability.
System Overview
The system incorporates 90-type two-frequency machine shaking laser gyroscope and quartz flexure accelerometer technologies. Advanced high-precision error calibration, temperature compensation, and dual-axis rotary on-line autonomous calibration with error self-compensation technologies significantly enhance system performance.
Through comprehensive electromagnetic shielding design, thermal balance optimization, vibration modal analysis, sealing design, and strict manufacturing processes, the system delivers excellent environmental adaptability for mission-critical operations.
Key Features
- High precision 90-type two-frequency machine shake laser gyroscope
- Dual-axis rotational self-calibration and error self-compensation
- Static base and moving base initial alignment capabilities
- Comprehensive error parameter calibration and compensation across full temperature range
- Preset GNSS/odometer/trip-meter interface compatibility
- Configurable for different navigation modes
- Excellent environmental adaptability
- Military standard compliance
Applications
- Ship navigation systems
- Underwater submarine navigation
- Positioning and orientation of missile launch vehicles
- High-precision attitude measurement
Performance Specifications
| Start-up time | 6 hours |
| 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℃ to +55℃ |
| Storage Temperature | -55℃ to +70℃ |
| Vibration | 0.04g²/hz @ 20-2000hz |
| Shock Resistance | Normal operation at 30g @ 6ms / No damage at 50g @ 11ms |
Electrical Characteristics
| Operating Voltage | 28VDC |
| Power Consumption | ≤200W |
| Communication Interface | RS422/RS232/CAN/Ethernet |
Physical Characteristics
| Dimensions (W * D * H) | φ550 * 500 mm |
| Weight | ≤60kg |
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