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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.

Multi-antenna Attitude Determination System MADS1000 1

MADS1000

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
GPS Aided Inertial Navigation System GINS3000 1

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
GNSS INS Integrate Navigation System GINS2000 1

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
GNSS INS Integrate Navigation System GINS1000 1

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

GNSS INS Integrate Navigation System GINS200 600

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
Multi-antenna-Attitude-Determination-System-MADS1000-1

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

GPS-Aided-Inertial-Navigation-System-GINS3000-1.jpg_2012009128

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

GNSS-INS-Integrate-Navigation-System-GINS2000-2

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

GNSS-INS-Integrate-Navigation-System-GINS1000-1.jpg_2012009128

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

GNSS-INS-Integrate-Navigation-System-GINS200-600.jpg_2012009128

GINS200 Low Cost GNSS/INS Integrated Navigation System

– Low Cost MEMS Inertial System with GPS/BD2 Dual-mode Satellite Navigation System

– High Accuracy: Heading: 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

– Power Supply: 9~36VDC

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

GNSS-INS-Integrated-Navigation-System-GINS100-1.jpg_2012009128

GINS100 Low Cost GNSS/INS Integrated Navigation System

– Low Cost MEMS Inertial System with GPS/BD2 Dual-mode Satellite Navigation System

– High Accuracy:

Heading: 0.5° (rms), Attitude: 0.5° (rms)

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

– Multiple Interface: RS422 / RS232 / TTL

– High Reliability, Strong Vibration Proof

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

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

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