GINS200
Integrated Navigation System
Digital Output
10dof
Yaw: 0.5deg; (RMS), Attitude: 0.3deg; (RMS)
ISO
Non-Customized
Ttl
5VDC
-40~85 Degrees Celsius
SkyMEMS
Carton
50*51.5*30mm
China
9014100000
Product Description
GINS200 Rugged Gnss Aided Itegraged Navigation System
Main Features
- 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
Brief Introduction
GINS200 Low Cost GNSS/INS Integrated Navigation System adopts MEMS inertial components and
integrates GPS/BD satellite navigation system.GINS200 has speical SkyMEMS new integrated navigation
fusion algorithm, which can realize high sensitivity tracking and accurate positioning in harsh environment.
The system enjoys smal 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, the surface craft, ship and so on.
Technical Specifications
Typical Applications
- unmanned aircraft
- vehicle navigation
- surface craft
- ship
Heart and Fast Service
Main Features
- 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
Brief Introduction
GINS200 Low Cost GNSS/INS Integrated Navigation System adopts MEMS inertial components and
integrates GPS/BD satellite navigation system.GINS200 has speical SkyMEMS new integrated navigation
fusion algorithm, which can realize high sensitivity tracking and accurate positioning in harsh environment.
The system enjoys smal 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, the surface craft, ship and so on.
Technical Specifications
| Parameter | Value | |
| Heading Accuracy | L1/B1 single point | 0.5°(rms) |
| Magnetic | 1°(rms) | |
| Attitude | Roll/Pitch accuracy | <0.3° degree (RMS) |
| Velocity | Velocity accuracy | <0.15m / s (RMS) |
| Position | Position accuracy | <5m (RMS) |
| Gyroscope | Range | ±300 °/s (ODM supported) |
| Bias stability | ≤8°/h (normal temperature, allan variance) | |
| Non-linearity | 0.0005 | |
| Bandwidth | 50Hz | |
| Accelerometer | Range | ±2g ~ ±20g |
| Bias stability | ≤5mg | |
| Random walk | ≤20µg (normal temperature, allan variance) | |
| Non-linearity | 0.0005 | |
| Receiver | Working mode | BD2 B1/GPS L1 |
| Cold start | 60s | |
| Warm start | 10s | |
| Electrical Specs | Power supply | 9~36VDC |
| Power consumption | ≤2.5W | |
| Startup Time | 3s | |
| Electrical interface | RS422 / RS232 / TTL | |
| Data refreshing rate | IMU: 100~400Hz; attitude: 100Hz | |
| Environment Conditions | Working temperature | -40~+80°C |
| Storage temperature | -40~+85°C | |
| Vibration | 6.06g (rms) | |
| Shock | 9g/11 ms, 1000g/1ms | |
| Physical Characteristics | Size | 50 × 51.5× 30mm |
| Weight | ≤100g | |
Typical Applications
- unmanned aircraft
- vehicle navigation
- surface craft
- ship
Heart and Fast Service
