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AND-EX9-1-A MEMS Aerial Reference System

The product consists of MEMS inertial measurement unit, together with the heading attitude a lgorithm and complementary filtering algorithm with completely independent intellectual property rights. By measuring the three-axis angular velocity and three-axis linear acceleration of the carrie r and calculating the pitch angle, roll angle and relative heading angle information, the product can output stable and reliable attitude information under dynamic environment.

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Product Details

Product Table

Parameters Unit Type
Heading angle drift (initial 0°, RMS) °/h 20
Pitch angle accuracy/roll angle accuracy (RMS) ° static:0.1
° dynamic:0.2
gyros Measurement range °/s ±400
Zero-bias stability (10s smo 1σ, room Temp) °/h 3
zero bias full Temp.(10s smo 1σ, room Temp) °/h 20
Zero bias repeatability °/h 3
Random Walk °/√h 0.15
Cross coupling % 0.1
accelerometer Measurement range g ±10
Zero-bias stability (10s smo 1σ, room Temp) mg 0.05
zero bias full Temp.(10s smo 1σ, room Temp) mg 2
Zero bias repeatability mg 0.2
Cross coupling % 0.1
Data update rate Hz 500(customisable)
Voltage V 3.3±0.33
Power consumption W 1.5
Operating Temperature -45~80
Dimension mm 47*44*14
Weight g 50
Interface —— TTL

FAQ

What are the quotation methods?

If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.

Are there any discounts?

After we submit the sample price, if more quantity is needed, we will quote the bulk price.

How long will it take to deliver the goods after placing the order?

For sensors, parts and modules: in a stock-one week; no stock-2-4 weeks; For systems, generally, 8-12 weeks.

How to deal with quality problems?

After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.

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