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IMU200

By Wuxi Beiwei Sensing Technology ↗

The Wuxi Beiwei Sensing Technology IMU200 is a low-cost inertial measurement unit for integration into unmanned aircraft, robotics and stabilization systems. It offers selectable serial interfaces, sampling up to 500 Hz, a 9–36 V DC supply range and compact unit and mainboard dimensions, with operation from -40 to +85 °C.

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Output interfacesRS232 / RS485 / TTLSelectable interface output.
External dimensionsL60 × W59 × H29 mm
Mainboard sizeL44 × W35 × H11 mmMainboard dimensions.
Supply voltage9–36 V DC
Operating temperature-40 to +85 °C
Maximum sampling frequencyUp to 500 Hz

Product overview

The Wuxi Beiwei Sensing Technology IMU200 provides inertial measurement for applications including unmanned aircraft, robots and platform stabilization. Its physical integration dimensions distinguish the complete unit, measuring 60 × 59 × 29 mm, from its 44 × 35 × 11 mm mainboard. Electrical integration uses a 9–36 V DC supply, with selectable RS232, RS485 or TTL output. These options define the available interface choices for incorporating the sensor into a host system.

The IMU200 combines gyroscope and accelerometer measurement with temperature, dynamic and orthogonality compensation. Sampling reaches up to 500 Hz, and operation spans -40 to +85 °C. Its precision figures carry distinct measurement conditions: gyroscope bias stability is specified at room temperature, while accelerometer bias stability uses 25 °C and separate 10-second and 100-second intervals. Procurement scope is an inertial measurement component for integration into a larger system; the product is neither a flight platform nor an airframe kit.

Specifications

SpecificationValue & conditions
Output interfacesRS232 / RS485 / TTLSelectable interface output.
External dimensionsL60 × W59 × H29 mm
Mainboard sizeL44 × W35 × H11 mmMainboard dimensions.
Supply voltage9–36 V DC
Operating temperature-40 to +85 °C
Maximum sampling frequencyUp to 500 Hz
Gyroscope bias stability, 100 sLess than 2 °/hRoom temperature; 100 s, 1σ.
Gyroscope bias stability, 10 sLess than 20 °/hRoom temperature; 10 s, 1σ.
Gyroscope angular random walk coefficientLess than 0.1 °/√h
Gyroscope bias repeatabilityLess than 50 °/h1σ.
Gyroscope scale factor nonlinearity≤ 100 ppm1σ.
Accelerometer resolution0.01 mg
Accelerometer bias0.15 mg
Accelerometer bias stability, 100 s0.001 mg25 °C; 100 s; 1σ.
Accelerometer bias stability, 10 s0.01 mg25 °C; 10 s; 1σ.
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