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Nanjing Sky MEMS Technology Co.,Ltd.
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IMU400 Mems Inertial Navigation System Fully Calibrated Temperature Compensated

IMU400 Mems Inertial Navigation System Fully Calibrated Temperature Compensated

Brand Name : SkyMEMS
Model Number : IMU400
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 IMU400 Inertial Measurement Unit
Application : Underwater Systems
Integrated sensors : Triaxial accelerometer, triaxial gyroscope
Accelerometer Range : ±10g (custom design)
Gyro Dynamic Range : ±150°/s
Magnetic sensor range : ±6gauss
Overload resistance : 2,000g
Startup time : ≤0.2s
Zero bias stability : accelerometer≤1mg/h; gyroscope≤30°/h
Zero repeatability : accelerometer≤1mg/h; gyroscope≤20°/h
Zero time drift : ≤1mV/h
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INS Navigation System MEMS Inertial Navigation System Inertial Measurement Unit for Underwater Systems IMU400


Product Description

IMU400 Inertial Measurement Unit is breakthrough, fully integrated inertial solutions that combine the latest MEMS sensors technology.

Fully calibrated, temperature compensated, mathematically aligned to an orthogonal coordinate system, IMU400 demonstrates less than 30 deg/hr gyroscopes and 0.001g accelerometers bias in-run stability with very low noise and high reliability.


Main Features

- High stability, high accuracy, high reliability, high survivability

- Small size, low weight and low cost

- Digital interface, RS232

- Fully calibrated, temperature-compensated

- Acceleration range:±10g, angular range:±150°/s, (custom design)

- Bias stability: acc 0.001g, gyro 30°/h

- Overload resistance: 2000g, IP67 protection

- Wide temperature: -40°C~+85°C

- Small size: 38*35*28mm


Typical Application

The IMU400 IMU is well suited for the applications in harsh environment, such as
- Aerospace and Defense applications
- UAVs, AUVs, AGVs, UGVs and ROVs
- Drone
- Control & Stabilization
- Navigation and correction
- Measurement & Testing
- Unmanned Contro
- Underwater Systems


Technical Specifications

Technical Specs
Angular rate Rangeacceleration:±10g, angular rate:±150°/s
Power supply5±0.25V
Current≤50mA
Output voltage0.1±0.1 V~4.9±0.1V
Startup time≤0.2s
Zero bias stabilityaccelerometer≤1mg/h; gyroscope≤30°/h
Zero repeatabilityaccelerometer≤1mg/h; gyroscope≤20°/h
Resolutionaccelerometer≤1mg; gyroscope≤0.1°/s
Zero time drift≤1mV/h
Zero output noise≤10mV
Weight≤50g
Dimension38*35*28mm
Working temperature-40~85°C
Overload resistance2000g

Competitive Advantages

High Performance Imu Inertial Measurement Unit

- High-quality components, industrial-grade MEMS only

- Excellent for control and stabilization

- Proven and robust filter design

- Overload resistance: 2,000g

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

- High cost effective


FAQ

What is Time Stamping / Synchronization?

Especially if an INS shall be used for control tasks or for surveying applications, a superior time stamping of the inertial data, odometer data and all other aiding information is mandatory. Therefore INS measurement systems also provide this feature with very high performance. If a target is moving with 100 m/s, a timing error of 1 milli second would already lead to a position error of 10 cm.

What is Open Interfaces?

Open interfaces are very important for the user to have highest flexibility in using the system. Interfaces are user-interfaces as well as interfaces to external sensors like GPS, odometer, depth/altitude sensor etc. The system's architecture should also provide custom specific interfaces if required. For higher volume markets the system shall be designed directly to these applications to meet the economical demands of those applications.


Product Tags:

inertial navigation unit

      

ins navigation system

      
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