High Performance GPS Ins Integrated Navigation System

Product Details
Customization: Available
Type: Integrated Navigation System
Output Signal Type: Digital Output
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Registered Capital
1000000 RMB
Plant Area
>2000 square meters
  • High Performance GPS Ins Integrated Navigation System
  • High Performance GPS Ins Integrated Navigation System
  • High Performance GPS Ins Integrated Navigation System
  • High Performance GPS Ins Integrated Navigation System
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Basic Info.

Model NO.
GINS200
Measuring Shaft Quantities
10dof
Accuracy Grade
Yaw: 0.5deg; (RMS), Attitude: 0.3deg; (RMS)
Certification
ISO
Customized
Non-Customized
Interface
Ttl
Power Supply
5VDC
Working Temperature
-40~85 Degrees Celsius
Transport Package
Carton
Specification
50*51.5*30mm
Trademark
SkyMEMS
Origin
China
HS Code
9014100000
Production Capacity
500/Month

Product Description

GINS200 Rugged Gnss Aided Itegraged Navigation System

High Performance GPS Ins Integrated 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


High Performance GPS Ins Integrated Navigation System
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.


High Performance GPS Ins Integrated Navigation System
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 

High Performance GPS Ins Integrated Navigation System
Typical Applications
- unmanned aircraft
High Performance GPS Ins Integrated Navigation System

- vehicle navigation
High Performance GPS Ins Integrated Navigation System

- surface craft
High Performance GPS Ins Integrated Navigation System

- ship

High Performance GPS Ins Integrated Navigation System


Heart and Fast Service
High Performance GPS Ins Integrated Navigation System


 

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