Cost-Effective Fiber Optic Inertial Navigation System If4010 for Fixed-Wing Survey Uav, Gnss+Ins Fusion, RS422 Data Link, Aviation Mapping, China Made

Customization: Available
After-sales Service: 1 Year
Warranty: 1 Year

Product Description

Basic Information

Model NO.
IF4010
Type
Bearing / Inertial Sensor
Application
Tunnel Boring Machine / Aerospace
Certification
CE
Weight
0.8kg
Supply Voltage
12~36V
Power Consumption
≤ 12W
Specification
33*27*8mm

Product Introduction

Inertial Navigation System: IF4010
The IF4010 is a FOG-40 type inertial measurement unit designed for high-precision technical requirements. This unit is widely utilized in vehicle-mounted, shipborne, and airborne applications, offering exceptional reliability and performance in demanding environments.

Inertial sensors are recognized for high precision, long operational life, and reliability across industries including aerospace, automotive, robotics, and consumer electronics. Strict production and factory inspection processes ensure each sensor meets stringent industrial standards.

Technical Specifications

Angular Velocity Measurement
Measurement Range± 300 °/s
Zero Bias Stability (Room Temp)≤ 0.8 °/h
Zero Bias Repeatability (Full Temp)≤ 0.8 °/h
Bandwidth≥300Hz
Start Time10 seconds
Linear Velocity Measurement
Acceleration Range± 20g (Optional 50g)
Zero Bias Stability≤ 200ug
Alignment & Navigation Accuracy
Heading Accuracy (Shaking Base)≤1.5 ° * secL
Pitch/Roll Accuracy≤0.05 °
Satellite Integrated Heading Accuracy≤0.3 ° (1 σ)
Horizontal Positioning Accuracy≤1.5 meters (1 σ)
Environmental Adaptability
Working Temperature-40 ℃ to +60 ℃
Storage Temperature-40 ℃ to +60 ℃

Dimensions & Definitions

Dimensions

Product Display

Product view 1
Product view 2
Product view 3
Integrated System Display

Frequently Asked Questions

Q1: What are the primary applications for the IF4010 system?
The IF4010 is a high-performance fiber optic gyroscope-based system used for vehicle-mounted, shipborne, and airborne navigation, providing precise angular and linear velocity data.
Q2: What is the measurement accuracy of the IF4010?
It offers an angular velocity zero bias stability of ≤ 0.8 °/h and a linear velocity zero bias stability of ≤ 200ug at room temperature.
Q3: How does the system handle satellite signal failure?
During satellite failure, the pure inertial navigation mode maintains heading drift accuracy at ≤1.5 °/h (peak) and pitch/roll drift at ≤1.0 °/h (peak).
Q4: What is the operating temperature range for this sensor?
The system is designed to operate reliably in extreme conditions, with a working and storage temperature range from -40 ℃ to +60 ℃.
Q5: Does the IF4010 support RTK and dual-antenna orientation?
Yes, the system supports receiving RTCM3.X data to enable RTK state and offers optional configurations for dual-antenna orientation.
Q6: What are the power and voltage requirements?
The system operates on a supply voltage of 12V to 36V with a power consumption of ≤ 12W.

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