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MEMS INS Sensor GPS Aided Inertial Navigation System For ROV INS300

MEMS INS Sensor GPS Aided Inertial Navigation System For ROV INS300

Brand Name : SkyMEMS
Model Number : INS300
Certification : CE, FCC, ROHS
Place of Origin : Nanjing, Jiangsu
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 INS300 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 : 200Hz
Operating Temperature : -40~85°C
Data storage capacity : 8GB
Output interface : RS232
Dimension : Φ80*85mm
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Pure Inertial MEMS INS Sensor GPS Aided Inertial Navigation System for ROV INS300

Product Description

INS300 Inertial Navigation System is an inertial navigation system providing position, true heading, attitude, speed, depth and heave. Its high-accuracy inertial measurement unit is based on SkyMEMS’s gyroscope technology coupled with an embedded digital signal processor that runs an advanced Kalman filter.

The system enjoys the advantages such as small size, light weight, low cost, low power consumption, quick start-up, high reliability, excellent adjustment in dynamic environment, it has been widely applied in tactical weapon, rocket measurement fields.

Main Features

- Real-time measure accurately the attitude angle, position, speed, acceleration and angular rate for high speed self-spinning flying body

High stability, high reliability, high survivability in harsh environment, 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: Φ80*85mm

Typical Application

INS300 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, INS300 has been widely applied in the special solutions, such as:

- Rocket

- Avionics

- Unmanned Ground Vehicle

- Tactical weapon

- Unmanned aircraft

- Robot Motion monitoring

- Targeting system


- 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 frequency200HzAdjustable
Data storage capacity8GB
Working Temperature-40~85°C
Overload resistance10,000g

Competitive Advantages

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

Experts in GNSS and inertial technology

Advanced algorithms in the Inertial+ combine the absolute positioning accuracy of GNSS with the stable orientation measurements of the inertial measurement unit to give a navigation solution that outperforms either technology. The Inertial+ can provide continuous position measurements free from jumps, even when satellite signals are blocked or obstructed. A wheel speed odometer can be used to reduce the drift even further.


a form of “Dead-Reckoning” that relies on accelerometers and gyroscopes to detect acceleration and velocity respectively along 3 perpendicular axes. An approximate 2 or 3 dimensional position can be constantly determined in relation to a known starting point, velocity and orientation.

also a term used to refer to the whole subject: theory, design, technology, and application.

Product Tags:

ins navigation system


strapdown inertial system

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