Product Model: NTFOG354A
Product Overview:
NTFOG354A Tri-Axis Closed-Loop Fiber Optic Gyroscope (FOG) Cluster.Designed for medium-to-low precision applications, this system employs a tri-axis shared-resource architecture to deliver cost efficiency and stable performance. Its optoelectronic co-packaged design integrates optical and electronic components into a single compact unit. When mounted in strapdown inertial navigation systems (INS), it measures angular rates of the vehicle relative to inertial space. Key features include small size, lightweight construction, and high-speed data output. The system is suitable for missile seekers, inertial navigation systems, unmanned aerial vehicles (UAVs), and robotic attitude monitoring platforms.
CLASSIFICATION ：TRI-AXIS FIBER OPTIC GYROSCOPE (FOG)
TAB：TRI-AXIS FIBER OPTIC GYROSCOPE (FOG)
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Tel: +86 18608017948(WeChat)
E-mail: marketing@newtron-tech.com
KEY FEATURE
- High Cost-Effectiveness & Economy
- High Integration & Compact Design
- Robust and Reliable Performance
- Low Power Consumption & High-Speed Output
APPLICATION SCENARIOS
- Missile Seekers
- Inertial Navigation Systems (INS)
- Unmanned Aerial Vehicles (UAVs)
- Robotic Attitude Monitoring Systems
PRIMARY FUNCTIONS
- Tri-Axis Angular Rate Measurement
- Providing Critical Sensing Data for Strapdown Inertial Navigation Systems (SINS)
- Platform Stabilization and Attitude Control
- Suitability for Cost-Sensitive Fields
SPECIFICATIONS
Table1: Basic Parameters
Performance Parameters | NTFOG354A |
Zero-Bias Stability | ≤1°/h(with 10-second averaging) |
Zero Bias Repeatability | ≤1°/h |
Random Walk Coefficient | <0.05°/√h |
Scale Factor Nonlinearity | ≤100ppm |
Scale Factor Repeatability | ≤100ppm |
Operating Temperature | -45°C ~ +65°C |
Dynamicrange | ≥±1000°/s |
Input Voltage | +5V |
Steady State Power Consumption | ≤5W |
External Dimension | 60mmx60mmx54mm |
Weight | ≤300g |
Note: All performance parameters and interfaces are customizable to mission requirements.
