PRODUCTS

  1. Home
  2. /
  3. PRODUCTS
  4. /
  5. INS
  6. /

Join Sunny not only provides high precision and low cost FOG/MEMS/DTG inertial navigation system (INS), inertial guidance system, inertial orientation system, inertial positioning system to the customers worldwide, but also customizes various inertial navigation system. The quality and after service are proven to be well guaranteed.

Current Type Triaxial Acceleration Sensor

Low Cost FOG INS

GSY-FINS-70 (0.3°):
1. Heading accuracy (1σ): ≤0.3°;
2. Attitude accuracy (1σ): ≤0.03°;
3. High performance & low cost.

Send Inquiry
Current Type Triaxial Acceleration Sensor

Integrated Navigation System

GSY-MINS-5610 (0.1°) Features:
1. Equipped with MEMS gyroscope and accelerometer and mapping multi-mode multi-frequency GNSS receiver;
2. It can achieve a single antenna dynamic alignment or dual antenna-assisted fast high-precision orientation;
3. The directional accuracy can reach up to 0.1 deg.

Send Inquiry
Current Type Triaxial Acceleration Sensor

MEMS Integrated Navigation System

GSY-MINS-5651 (0.1°) Features:
1. Equipped with MEMS gyroscope and accelerometer and mapping multi-mode multi-frequency GNSS receiver;
2. It can achieve a single antenna dynamic alignment or dual antenna-assisted fast high-precision orientation;
3. The directional accuracy can reach up to 0.1 deg.

Send Inquiry
Current Type Triaxial Acceleration Sensor

High Performance FOG INS

GSY-FINS-98 (0.1°secψ):
1. Azimuth accuracy ≤ 0.1° secψ (1σ);
2. Attitude accuracy ≤ 0.02° (1σ);
3. Azimuth holding accuracy ≤ 0.05°sec lat (1σ).

Send Inquiry
Current Type Triaxial Acceleration Sensor

MEMS Inertial Navigation System

GSY-MINS-210/230 (0.3~1.0°) Features:
1. Provide horizontal attitude, heading attitude, longitude, latitude, altitude, etc;
2. Can be widely used in unmanned aerial vehicles, vehicle navigation, aviation and platform stability control and other fields.

Send Inquiry
Current Type Triaxial Acceleration Sensor

High Precision FOG INS

GSY-FINS-120 (0.01°):
1. Heading accuracy (1σ): ≤0.01°;
2. Attitude accuracy (1σ): ≤0.01°;
3. Positional accuracy (1σ): 1.0nm/2h.

Send Inquiry
Current Type Triaxial Acceleration Sensor

MEMS Integrated INS

GSY-MINS-5680 (0.5°) Features:
1. 0.1° (dynamic alignment);
2. 0.5° (low dynamic dual antenna assistance, 2m baseline);
3. Support fast and high precision orientation up to 0.1 °.

Send Inquiry
Current Type Triaxial Acceleration Sensor

Dynamically Tuned Inertial Navigation System

GSY-DINS-1 (0.4~0.5°) Features:
1. Strapdown inertial navigation system determination of aircraft position, heading, altitude;
2. System with emergency rapid alignment, normal alignment, navigation, correction, parameter calibration, testing, parameter binding, non volatile storage.

Send Inquiry
Menu