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GNSS/INS is the hybrid navigation system that merges Global Navigation Satellite System (GNSS) and Inertial Navigation System (INS) to provide continuous, as well as precise positioning and attitude information. GNSS uses satellite signals for global positioning; INS employs accelerometers and gyroscopes built into its mechanism for self-sensing, motion tracking without reliance on any external signal. The integration of such technologies within a single system enables not only high-precision navigation but also seamless relaying whenever satellite signals become restricted or interrupted so that continuity and stability in navigation can be maintained.

GNSS/INS delivers greater robustness in navigation when compared with standalone systems, and, consequently, environmental adaptability. It can use the INS for the duration that is characterized by intense blockage of satellite signals in such places as city streets, tunnels, forests, and even underwater to guarantee system failure will not occur. When the satellite signal returns fusion algorithm immediately corrects accumulated errors from INS thus making long-term stability much better as well as accuracy of navigation data overall.

GNSS/INS fused navigation finds its applications in aircraft, land-based autonomous vehicles, marine vessels, agricultural machinery navigators, surveyors, and mappers. Intelligent transportation, precision agriculture, and unmanned system development give rise to systems demanding such high levels of accuracy along with reliability and latency in data output-from centimeter level positioning to complex trajectory tracking. GNSS/INS will continue to be the core enabler of intelligent perception and high-precision navigation systems as long as fusion algorithms and sensor technologies are constantly upgraded.

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

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

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

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

– 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

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

– 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

– 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

– 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

– 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

Starts from the Best Quality

Product Categories

MADS1000 Determination System

GINS3000 Airborne GPS Aided Inertial System

GINS2000 Rugged GNSS Aided Inertial System

GINS1000 Single Antenna Integrated Navigation System

GINS100 Embedded GPS Inertial Navigation System

GINS200

MADS1000 Multi-antenna Attitude Determination System

GINS3000 High Performance GNSS/INS Integrated Navigation System

GINS2000 High Performance GNSS/INS Integrated Navigation System

GINS1000 High Performance GNSS/INS Integrated Navigation System

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