GINS100
Integrated Navigation System
Digital Output
10dof
Yaw: 0.5deg; (RMS), Attitude: 0.5deg; (RMS)
ISO
Non-Customized
Ttl
5VDC
SkyMEMS
Carton
43* 37*15mm
China
9014100000
Product Description
GINS100 Low Cost Integrated Navigation System
Main Features
- 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
Brief Introduction
GINS100 Low Cost GNSS/INS Integrated Navigation System provides outstanding orientation and position
data in small, light-weight board, which adopts MEMS inertial components and integrates GPS/BeiDou
satellite navigation system. GINS100 is composed of 3 axis accelerometers, 3 axis gyroscopes, 3 axis
magnetometers, 1 barometer, GNSS receiver and high performance CPU, etc. and GINS100 adopts
advanced SkyMEMS integrated navigation fusion algorithm, which can realize high sensitivity tracking and
accurate positioning in harsh environment.
The system enjoys small size, light weight, low cost, and low power consumption, fast start-up, and high
reliability. It has been widely used in unmanned aircraft, vehicle navigation, surface vessel, ship and so on.
Technical Specifications
Typical Applications
- unmanned aircraft
- vehicle navigation
- surface craft
Heart and Fast Service
Main Features
- 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
Brief Introduction
GINS100 Low Cost GNSS/INS Integrated Navigation System provides outstanding orientation and position
data in small, light-weight board, which adopts MEMS inertial components and integrates GPS/BeiDou
satellite navigation system. GINS100 is composed of 3 axis accelerometers, 3 axis gyroscopes, 3 axis
magnetometers, 1 barometer, GNSS receiver and high performance CPU, etc. and GINS100 adopts
advanced SkyMEMS integrated navigation fusion algorithm, which can realize high sensitivity tracking and
accurate positioning in harsh environment.
The system enjoys small size, light weight, low cost, and low power consumption, fast start-up, and high
reliability. It has been widely used in unmanned aircraft, vehicle navigation, surface vessel, ship and so on.
Technical Specifications
| Parameter | Value | |
| Heading Accuracy | L1/B1 single point | 0.5°(rms) |
| Magnetic based | 1°(rms) | |
| Attitude | Roll/Pitch accuracy | <0.5° degree (RMS) |
| Velocity | Velocity accuracy | <0.15m / s (RMS) |
| Position | Position accuracy | <5m (RMS) |
| Gyroscope | Range | ±300 °/s (ODM supported) |
| Bias stability | ≤10°/h (normal temperature, allan variance) | |
| Non-linearity | 0.0005 | |
| Bandwidth | 50~200Hz | |
| Accelerometer | Range | ±5g |
| Bias stability | ≤5mg | |
| Non-linearity | 0.05% (full scale) | |
| Magnetic Sensor | Range | 6Gauss |
| Resolution | 120uGauss | |
| In band noise(RMS) | 50uGauss | |
| Barometer | Range | 1100mbar |
| Resolution | 0.1mbar | |
| GNSS Receiver | Working mode | GPS L1 C/A, GLONASS L10F, BeiDou B1 |
| Cold start | 26s | |
| Warm start | 10s | |
| Electrical Specs | Power supply | 5VDC±5% |
| Power consumption | ≤1W | |
| Startup Time | 3s | |
| Electrical interface | TTL | |
| Data refreshing rate | 100Hz | |
| Environment Conditions | Working temperature | -40~+70°C |
| Storage temperature | -55~+85°C | |
| Vibration | 6.06g (rms) | |
| Shock | 9g/11 ms, 1000g/1ms | |
| Physical Characteristics | Size | 43 × 37× 15mm (without casing) |
| Weight | ≤20g (without casing) | |
Typical Applications
- unmanned aircraft
- vehicle navigation
- surface craft
Heart and Fast Service
