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GNSS/INS is a hybrid navigation system that combines the use of Global Navigation Satellite Systems (GNSS) with an Inertial Navigation System (INS). GNSS is a satellite-based navigation system that allows a receiver to determine its location by receiving signals from multiple satellites. INS is a self-contained system that uses accelerometers and gyroscopes to measure the movement of an object and calculate its position and orientation. By combining the two systems, GNSS/INS can provide highly accurate and reliable navigation information in a variety of environments, including areas where GNSS signals may be weak or unavailable. GNSS/INS is commonly used in applications such as aviation, marine navigation, and autonomous vehicles.

MADS1000

MADS1000 Determination System

highly precise attitude determination system, based on 4 groups of GNSS receivers, widely used in the surface craft.

  • Built-in Mini AHRS soft/hardware
  • Yaw, Roll, Pitch, Acceleration and Angular Rate Outputs
  • High Accuracy: Yaw: 0.2° , Attitude: 0.1° (base line≥1m)
  • RS232/RS422 Interface, 100Hz /200Hz Output Rate
  • High Reliability, Strong Vibration and Shock Proof
  • Advanced SkyMEMS Data Fusion Algorithm
  • Wide Operating Temperature: -40°C~+85°C
GINS3000 Airborne GPS Aided Inertial System

GINS3000 Airborne GPS Aided Inertial System

high-performance airborne GPS aided inertial system, widely used in unmanned aircraft, vehicle navigation, surface craft, ship, and so on.

  • High-Performance MEMS Inertial System with GPS/GLONASS Satellite Navigation System
  • High Accuracy: Yaw: 0.5° (1σ), Attitude: 0.23° (1σ), Velocity <0.05~0.1m/s, Position < 5m (L1/L2 single point), <8cm (RTK), Heave: <15cm (1σ)
  • RS422 Interface, 100Hz Data Output Rate
  • High Reliability, Strong Vibration Proof
  • Advanced SkyMEMS Data Fusion Algorithm
GINS2000 Rugged GNSS Aided Inertial System

GINS2000 Rugged GNSS Aided Inertial System

High Performance rugged GNSS aided inertial system, widely used in tactical weapon, unmanned aerial vehicle (UAV), ship, etc.

  • 3 Systems, 6 Frequency GNSS
  • High Tracking Sensitivity for Complicated Environment
  • High Accuracy: yaw up to 0.1°, Attitude: 0.1° (rms), Velocity <0.03m/s, Position < 0.01m (RMS, RTK),
  • High Reliability, Strong Vibration and Shock Resistance
  • Multiple Interfaces: RS232 / RS422 /TTL
  • Adjustable Bandwidth and Protocol ODM Supported
GINS1000 Single Antenna Integrated Navigation System

GINS1000 Single Antenna Integrated Navigation System

High precision integrated navigation system, widely used in unmanned aerial vehicle (UAV), vehicle navigation, the surface craft, ship and so on.

  • High Precision MEMS Inertial System with GPS/BD Dual-mode Satellite Navigation System
  • High Accuracy: Heading: 0.15°(rms), Attitude: 0.05° (rms), Velocity <0.15m/s, Position < 1.5m
  • Support Dynamic Fast Alignment
  • High Reliability, Strong Vibration and Shock Resistance
  • Multiple Interfaces: RS232/RS422/TTL/CAN
  • Easy to Integrate with Odometer/DVL Sensor
GINS100 Embedded GPS Inertial Navigation System

GINS100 Embedded GPS Inertial Navigation System

GINS100 Embedded GPS Inertial Navigation System

– Low-Cost MEMS GNSS/INS System with GPS/BeiDou

Dual-mode Satellite Navigation System

– High Accuracy: Yaw: 0.5° (RMS), Attitude: 0.5° (RMS)

Velocity <0.15m/s, Position < 5m (RMS)

– Up to 400Hz Output Rate

– High Reliability, Strong Vibration Proof

– Small Size: 43 × 37× 15mm, 20grams (without casing)

– Wide Operating Temperature: -40°C~+70°C

GINS200

GINS200

Low-cost GNSS/INS integrated navigation system, widely used in unmanned aircraft, vehicle navigation, surface vessel, ship and so on.

  • Low-Cost MEMS Inertial System with GPS/BD2 Dual-mode Satellite Navigation System
  • High Accuracy: Yaw: 0.5° (rms), Attitude: 0.3° (rms), Velocity <0.15m/s, Position < 5m (rms)
  • Multiple Interface: RS422 / RS232 / TTL
  • High Reliability, Strong Vibration Proof
  • Small Size: 50 × 51.5× 30mm, <100grams
  • Wide Operating Temperature: -40°C~+80°C
MADS1000 Multi-antenna Attitude Determination System

MADS1000 Multi-antenna Attitude Determination System

– Built-in Mini AHRS soft/hardware

– Yaw, Roll, Pitch, Acceleration and Angular Rate Outputs

– High Accuracy: Yaw: 0.2° , Attitude: 0.1° (base line≥1m)

– RS232/RS422 Interface, 100Hz /200Hz Output Rate

– High Reliability, Strong Vibration and Shock Proof

– Advanced SkyMEMS Data Fusion Algorithm

– Wide Operating Temperature: -40°C~+85°C

GINS3000 High Performance GNSS/INS Integrated Navigation System

GINS3000 High Performance GNSS/INS Integrated Navigation System

– High Performance MEMS Inertial System with GPS/GLONASS Satellite Navigation System

– High Accuracy: Yaw: 0.5° (1σ), Attitude: 0.23° (1σ), Velocity <0.05~0.1m/s,

Position < 5m (L1/L2 single point), <8cm (RTK), Heave: <15cm (1σ)

– RS422 Interface, 100Hz Data Output Rate

– High Reliability, Strong Vibration Proof

– Advanced SkyMEMS Data Fusion Algorithm

GINS2000 High Performance GNSS/INS Integrated Navigation System

GINS2000 High Performance GNSS/INS Integrated Navigation System

– High Precision MEMS Inertial System with GPS/BD Dual-mode Satellite Navigation System

– 3 System, 6 Frequency GNSS

– High Tracking Sensitivity for Complicated Environment

– High Accuracy: Heading up to 0.1°, Attitude: 0.1° (rms),

Velocity <0.03m/s, Position < 0.01m (RMS, RTK),

– High Reliability, Strong Vibration and Shock Resistance

– Adjustable Bandwidth and Protocol ODM Supported

– Wide Operating Temperature: -40°C~+80°C

GINS1000 High Performance GNSS/INS Integrated Navigation System

GINS1000 High Performance GNSS/INS Integrated Navigation System

– High Precision MEMS Inertial System with GPS/BD Dual-mode Satellite Navigation System

– High Accuracy: Heading: 0.15°, Attitude: 0.05° (rms), Velocity <0.15m/s, Position < 1.5m

– Support Dynamic Fast Alignment

– High Reliability, Strong Vibration and Shock Resistance

– Multiple Interfaces: RS232/RS422/TTL/CAN

– Eazy to Integrate with Odometer/DVL Sensor

– Wide Operating Temperature: -40°C~+70°C

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