Aerospace FOG INS (INT-M-A05) for UAV and Aircraft Navigation Solution

The INT-M-A05 is an airborne fiber-optic inertial navigation system (FOG-INS) designed for UAVs and special aircraft. It utilizes optical gyroscopes and quartz accelerometers as core inertial sensors and adopts a strapdown architecture.
The system runs high-speed internal navigation software to compute and output real-time inertial navigation data, including attitude, heading, velocity, and position.
According to user requirements, the Merak-A05 supports pure inertial navigation as well as multi-sensor integrated navigation, enabling fusion with GNSS, altimeters, radio navigation, vision, and other external aiding sources.

Key Advantages

• Airborne-grade optical gyroscope for stable inertial measurement
• Strapdown configuration reduces weight and improves integration efficiency
• Supports pure inertial and integrated navigation
• Real-time computation and data output
• Compatible with multi-source aiding sensors
• Suitable for UAV platforms with space/power constraints

Applications
✔ Unmanned Aerial Vehicles (UAVs)
✔ Special-purpose aircraft (e.g., survey, research, and tasks requiring stabilized navigation)

These platforms benefit from high-quality inertial data during flight where accurate position, attitude, and heading information is required.