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Nanjing Sky MEMS Technology Co.,Ltd.
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INS Sensor Boat Navigation System For Vessels / Ships OEM / ODM Available

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

INS Sensor Boat Navigation System For Vessels / Ships OEM / ODM Available

Brand Name : SkyMEMS
Model Number : GINS200
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 : Vessels and Ships
Roll/Pitch accuracy : <0.3 degree (RMS)
Position accuracy : 5m (RMS)
Speed accuracy : <0.15m / s (RMS)
Receiver Working mode : BD2 B1/GPSL1
MTBF : 10000 hours
Power supply capacity : 7~30VDC
Power consumption : ≤2.5W
Electrical interface : RS232/RS422
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Boat Navigation System INS Sensor Integrated Navigation System for Vessels and Ships Applications GINS200


Product Description

GINS200 GNSS/INS Integrated Navigation System adopts high precision MEMS inertial components and integrates GPS/BD single frequency dual-mode satellite navigation system. It has built-in magnetic heading measurement system and has the height measurement solution. GINS200 has speical SkyMEMS new integrated navigation fusion algorithm, which can realize high sensitivity tracking and accurate positioning in open space, and it also can realize navigation application in the city, forest, canyon terrain, etc.

GINS200 GNSS INS Integrated Navigation System.pdf


Main Features

- Low Cost Compact MEMS inertial system with GPS/BD dual-mode satellite navigation system

- High Reliability, strong vibration proof

- High performance, position accuracy <5m, speed accuracy<0.15m/s, attitude accuracy: 0.3° (rms)

- Rich external interface:RS232/RS422, protocol optional

- Smaller size, lighter weight, lower cost

- Wide temperature: -40°C~+60°C


Typical Application

GINS200 Integrated Navigation System enjoys high performance and has been widely applied in the special solutions, such as:

- Mid-sized & large UAV

- Avionics

- Vessels, Ships

- Helicopters


Technical Specifications


Technical Specs
NameValue
AttitudeRoll/Pitch accuracy<0.3 degree (RMS)
PositionPosition accuracy5m (RMS)
SpeedSpeed accuracy<0.15m / s (RMS)
GyroscopeRange±400 °/s
Scale factor Non-linearity1000ppm
Zero Bias stability≤50°/h
Zero Bias repeatability≤200°/h
Bandwidth50~200Hz
AccelerometerRange±2~ ±10g
Bias≤3mg
Bias instability≤8mg (Allan variance)
Non-linearity (full range)0.05%
In Band Noise0.5°/s
ReceiverWorking modeBD2 B1/GPSL1
MTBF10000 hours
Electronic specsPower supply7~30VDC
Power consumption≤2.5W
Electrical interfaceRS232/RS422
Output rate100~400Hz
Environment conditionsWorking temperature-40~+60°C
Storage temperature-55~+85°C
Vibration6g @ 20~2000 Hz
Shock9g/11 ms, 1000g/1ms
Physical characteristicsSize58 × 45× 30mm
Weight≤100g

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

- High cost effective


FAQ

What is Correction of the Inertial Navigation Solution?

The integrated navigation solution of an INS/GNSS integrated navigation system is the corrected inertial navigation solution. In a conventional integration architecture using an error-state Kalman filter and separate inertial navigation processing, correction

may be either open-loop or closed-loop, regardless of what type of GNSS measurements are used and how the GNSS user equipment is aided.

In the open-loop configuration, the estimated position, velocity, and attitude errors are used to correct the inertial navigation solution within the integration algorithm at each iteration but are not fed back to the INS. Consequently, only the integrated navigation solution contains the Kalman filter estimates, and a raw

INS solution is available for use in integrity monitoring. Either

the raw INS or integrated navigation solution may be used for GNSS aiding.


Product Tags:

ins navigation system

      

mems inertial sensors

      
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INS Sensor Boat Navigation System For Vessels / Ships OEM / ODM Available Images

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