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Nanjing Sky MEMS Technology Co.,Ltd.
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Compact Design Integrated Navigation System For UAV Unmanned Aerial Vehicle GINS100

Nanjing Sky MEMS Technology Co.,Ltd.
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Nanjing Sky MEMS Technology Co.,Ltd.
City: Nanjing
Province/State: Jiangsu
Country/Region: China
Tel: +86-25-83356968
Contact Person:
Mr David zhu

Compact Design Integrated Navigation System For UAV Unmanned Aerial Vehicle GINS100

Brand Name : SkyMEMS
Model Number : GINS100
Certification : CE, FCC, ROHS
Place of Origin : Nanjing, Jiangsu
MOQ : 1PCS
Price : discuss personally
Payment Terms : Western Union, MoneyGram, L/C, T/T, D/A, D/P
Supply Ability : 1000PCS for month
Delivery Time : 3-5 days after payment
Packaging Details : Strong carton with PET strap for GINS100 Integrated Navigation System
Application : Unmanned Aerial Vehicle
Accelerometer Range : <100m (Within 100s)
Power supply : DC +7V~+15VDC
Attitude angle error : ≤2°
Output interface : RS232
Data refresh frequency : 200Hz (Adjustable)
Data storage capacity : 8GB
Weight : 10,000g
Overload resistance : 10,000g
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INS Sensor GNSS INS Integrated Navigation System for UAV Unmanned Aerial Vehicle GINS100


Product Description

GINS100 GNSS/INS integrated navigation system is composed of 3-axis MEMS accelerometers, 3-axis MEMS gyroscopes and GNSS satellite navigation system, it adopts real-time operating system and has special data fusion filtering algorithm in the high-performance information processing CPU, the system can have good response and provide reliable and accurate attitude parameters in the static, dynamic and shock environment.

The system enjoys smaller size, lighter weight, lower cost, and lower power consumption, faster start-up, and higher reliability, better dynamic environment adjustment, etc. It can be applied in tactical weapon, unmanned aircraft fields.


Main Features

- High Performance Integrated Navigation Systems

- High stability, high reliability, high survivability in harsh environment, fully calibrated INS

- Provide accurately real-time 3D position, speed, acceleration, attitude angle, angular rate, etc.

- Position accuracy of pure inertial navigation: 100m (100s)

- Attitude angle error: 2°, data refresh frequency: 200Hz

- Overload resistance:10000g, IP67 protection

- Wide temperature: -40°C~+85°C

- Small size: 60*60*60mm


Typical Application

GINS100 Integrated Navigation System can measures the complete motion. And it enjoys high overload resistance up to 10000g, GINS100 has been widely applied in the special solutions, such as:

- Mid-sized & large UAV

- Avionics

- Unmanned Ground Vehicle

- Motion monitoring

- AUV, ROV

- Weapon


Technical Specifications

Technical Specs
NameTechnical specsRemarks
Position accuracy of pure inertial navigation<100mWithin 100s
Attitude angle error≤2°
Power supplyDC +7V~+15VDC
Output interfaceRS232
Data refresh frequency200HzAdjustable
Data storage capacity8GB
Weight400±20g
Dimension60*60*60mm
Working Temperature-40~85°C
Overload resistance10,000g

Competitive Advantages

High Performance Integrated Navigation System

- Highly accurate, reliable and temperature stable

- Advanced, extendable, embedded Kalman Filter based sensor fusion algorithms

- State-of-the-art algorithms for different dynamic motions of Vessels, Ships, Helicopters, UAV, UUV, UGV, AGV, ROV, Gimbals and Land Vehicles

- Full temperature calibration of all sensing elements.

- Environmentally sealed (IP67), compact design

- Overload resistance: 10,000g

- Full tests and individual calibration from -40 to 85°C

- High cost effective


FAQ

What is Complementary Nature of GNSS and INS?

GNSS and INS systems are complementary in many aspects, shortly described below.

INS short-term errors are relatively small, but they degrade rapidly and are unbounded and so external aiding is necessary . On the other hand GNSS systems are more stable in long-term, meaning their errors are effectively time invariant with homogeneous accuracy . Hence GNSS systems can be used as external aiding to bound INS errors.

INS can provide accurate short-term data with very high rate and can be used to interpolate GNSS trajectory. In addition INS sensors supply data with continuity, while GNSS are subject to outages, caused by signal blocking or interference. For this reasons high-precision inertial sensors (as tactical or superior grade) can be used to bridge GNSS outages; unfortunately this might be not possible with MEMS sensors owing to their large error drift.

Finally INS systems provide the complete navigation state, including position, velocity and attitude while a single GNSS receiver cannot supply angular information.


Product Tags:

ship navigation system

      

mems inertial sensors

      
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