GSINS032C Flagship FOG Navigation System
GSINS032C sets the benchmark with gyro bias ≤0.005°/h, pure inertial positioning <0.5nm/h, attitude <0.005°, and north-seeking <0.03°secφ. Integrates full multi-constellation GNSS with DVL and odometer fusion. Dual RS232, dual RS422, CAN, and RJ45 interfaces ensure compatibility with any system architecture. At 5kg, this flagship system is built for strategic-grade navigation and precision survey missions where failure is not an option.
Feature:
● High-Precision Angular Velocity Measurement
● Strong Anti-Interference Capability
● Compact and Lightweight, Suitable for Space-Constrained Applications
● No Mechanical Wear, Longer Service Life
● Rich Interfaces, Compatible with DVL, Odometer, and USBL
● High-Precision Angular Velocity Measurement
● Strong Anti-Interference Capability
● Compact and Lightweight, Suitable for Space-Constrained Applications
● No Mechanical Wear, Longer Service Life
● Rich Interfaces, Compatible with DVL, Odometer, and USBL
5.0
design customization
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Please fill out the form below to request a quote or to request more information about us. please be as detailed as possible in your message, and we will get back to you as soon as possible with a response. we're ready to start working on your new project, contact us now to get started.
Product Introduction
A fiber optic inertial integrated navigation system integrates an Inertial Navigation System (INS) with other navigation systems such as the Global Navigation Satellite System (GNSS). By using algorithms like Kalman filtering, it fully leverages the advantages of the inertial navigation system—high short-term accuracy and strong autonomy—and the global navigation satellite system—stable long-term accuracy. This integration suppresses the respective errors of each system, achieves optimal calculation of the carrier's position, velocity, and attitude, and enhances the reliability and stability of the navigation system.
The fiber optic inertial integrated navigation system consists of an Inertial Measurement Unit (IMU), a satellite navigation receiver, a navigation computer, and a data transmission interface.
The GSINS032C Fiber Optic Inertial Integrated Navigation System is a miniaturized fiber optic inertial integrated navigation system with a volume of only 167*137*128mm and a weight of merely 5kg. Composed of a 3-axis integrated fiber optic gyroscope, a quartz accelerometer, and a full-system multi-frequency satellite module, this system is widely used in the navigation and attitude measurement of aerospace vehicles, unmanned vehicles, and ships.
Technical Specifications
| Specification Category | Specification Parameter | GSINS032C |
| Power Supply | Input Voltage | 18~36VDC |
| Power Voltage | <5s | |
| Power 25°C | <20W | |
| Navigation Parameters | Position Accuracy | <0.5nm/h;<0.15%*D(DVL);<0.1%*D(ODO) |
| Attitude Accuracy (Pitch & Roll Accuracy) | <0.005° | |
| North-Seeking Accuracy | <0.03°secφ | |
| Heading Accuracy | <0.03° | |
| RTK | <2cm+1ppm | |
| Single Point Positioning | <1.2m | |
| Velocity Accuracy | <0.02m/s (GNSS-INS Combo) | |
| Initialization Time | <1-2min | |
| Gyroscope Parameters | Bias | ±1000 °/s |
| Bias stability | ≤ 0.005°/h | |
| IMU Parameters | Bias | ±30 g |
| Bias stability | ≤ 30μg | |
| Environmental | Operating temperature | -45~+70°C |
| Storage temperature | -55~+80°C | |
| Other Specifications | Output | 2×RS232, 2×RS422, 1×PPS, 1×CAN, 1×RJ45 |
| Data update rate | 0.1-100Hz | |
| Weight | <5kg | |
| Size | 167×137×128mm |
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Application
- Aircraft Attitude Control, Navigation and Positioning
- Autonomous Vehicle Positioning and Path Planning
- Robot Attitude Control and Motion Tracking.
Our in-house designers and engineers have produced countless great designs for customers from different industries
- Navigation and Positioning for Ships, Submarines and
Underwater Robots (ROVs/AUVs)
- Missile Guidance
Our in-house designers and engineers have produced countless great designs for customers from different industries
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Since 2008, Gyrosens has been committed to delivering reliable and accurate motion sensing and navigation products, including gyroscopes, accelerometers, IMUs (Inertial Measurement Units), and AHRS (Attitude and Heading Reference Systems).
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