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3d Position Sensor Without GPS , Ins Navigation System For Unmanned Aircraft

3d Position Sensor Without GPS , Ins Navigation System For Unmanned Aircraft

Brand Name : SkyMEMS
Model Number : INS200
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 cartn with PET strap for INS200 Inertial Navigation System
High Performance Inertial Navigation System : Yes
Position accuracy of pure inertial navigation : <100m within 100seconds
Attitude Angle Error : ≤2°
Overload Resistance : 10000g
Power supply : +7V~+15VDC
Data refresh frequency : 1000Hz
Operating Temperature : -40~85°C
Factory Calibrated : Yes
Output interface : RS232
Dimension : 50*40*30mm
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Compact 3D Position INS System Inertial Navigation System without GPS Aided for Unmanned Aircraft INS200


Product Description

INS200 Inertial Navigation System is composed of MEMS accelerometer, MEMS gyroscope and high-performance information processing circuit and system functional module, it is mainly used to measure 3D position, speed, acceleration, attitude angle, and angular rate, etc.

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 get better performance to work with GPS and BEIDOU satellite position system, and it can be applied in tactical weapon, unmanned aircraft, robot fields.

INS200 Inertial Navigation System.pdf


Main Features

- High Performance Inertial Systems

- High stability, high reliability, high accuracy

- Fully calibrated INS

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

- Attitude angle error: 2°

- Overload resistance:10000g,

- IP67 protection

- Wide temperature: -40°C~+85°C,

- small size: 50*40*30mm


Typical Application

INS200 Inertial Navigation System can provide accurately real-time 3D position, speed, acceleration, attitude angle, angular rate, etc., which measures the complete motion. And it enjoys high overload resistance up to 10000g, INS200 has been widely applied in the special solutions, such as:

- Mid-sized & large UAV

- Avionics

- Unmanned Ground Vehicle

- Tactical weapon

- Unmanned aircraft

- Robot Motion monitoring

- Targeting system

- AUV, ROV

- SATCOM antenna

- Machine Control

- 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 frequency1000HzAdjustable
Weight≤150g
Dimension50*40*30mm
Working Temperature-40~85°C
Overload resistance10,000g

Competitive Advantages

High Performance INS Inertial Navigation System

High Performance INS Inertial Navigation System

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

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

- 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 the Applications of Inertial Navigation System (INS)?

Inertial navigation systems are used in many different moving objects, including vehicles—such as aircraft, submarines, spacecraft—and guided missiles. However, their cost and complexity place constraints on the environments in which they are practical for use.


Product Tags:

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