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Archimedes Innovation AIM-4930R MEMS inertial sensor with gold-colored housing and mounting flangeArchimedes Innovation AIM-4930R MEMS inertial sensor with gold-colored housing and mounting flange

AIM-4930R

The Archimedes Innovation AIM-4930R is a compact six-axis MEMS inertial sensor for UAVs, robotics, surveying, stabilization platforms and other unmanned systems. Configurable hardware and software options accompany industry-standard communication interfaces, ±400 °/s gyroscope and ±30 g accelerometer measurement ranges, and a maximum update rate of 2000 Hz.

Archimedes InnovationDrone flight controller
Weight
130 ± 10 g
Dimensions
64.8 × 47 × 35.3 mm

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Product overview

The Archimedes Innovation AIM-4930R is a six-axis MEMS inertial sensor for agriculture, AUVs, robotics, surveying, stabilization platforms, UAVs and unmanned ground vehicles. Its hardware and software options allow configuration according to application requirements, while industry-standard communication interfaces support integration into different architectures. The compact unit measures 64.8 × 47 × 35.3 mm and weighs 130 ± 10 g. It operates from a 5~12 V supply, with steady-state power consumption of ≤2 W.

The AIM-4930R combines a gyroscope measurement range of ±400 °/s with an accelerometer measurement range of ±30 g. Both have bandwidths of ≥200 Hz and cross coupling of ≤0.001 rad. Startup takes ≤2 s, and the maximum update rate is 2000 Hz. The operating temperature range is -40 to +80 °C, with storage from -55 to +85 °C. Environmental specifications include vibration of 6.06 g RMS over 20~2000 Hz and shock of 500 g for 1ms.

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Specifications

AIM-4930R specifications
SpecificationValue & conditions
Product identity and configurationArchimedes Innovation AIM-4930R six-axis MEMS inertial sensor, configurable with different hardware and software options.
Applications and integration featuresApplications include agriculture, AUVs, robotics, surveying, stabilization platforms, UAVs and unmanned ground vehicles. Compact, lightweight, low-power construction with industry-standard communication interfaces.
Gyroscope measurement range±400 °/s
Gyroscope bias≤2 °/hFull temperature; 3σ.
Gyroscope bias stability≤0.5 °/h10 s smoothing.
Gyroscope bias instability≤0.05 °/hAllan; typical.
Gyroscope bias repeatability≤0.3 °/h
Gyroscope angle random walk≤0.02 °/√h
Gyroscope scale factor nonlinearity≤100 ppm
Gyroscope cross coupling≤0.001 rad
Gyroscope bandwidth≥200 Hz
Accelerometer measurement range±30 g
Accelerometer bias≤2 mgFull temperature; 3σ.
Accelerometer bias stability≤50 µg10 s smoothing.
Accelerometer bias instability≤30 µgAllan; typical.
Accelerometer bias repeatability≤50 µg
Accelerometer velocity random walk≤0.03 m/s/√h
Accelerometer scale factor nonlinearity≤100 ppm±1 g.
Accelerometer cross coupling≤0.001 rad
Accelerometer bandwidth≥200 Hz
Power supply5~12 V
Power consumption≤2 WSteady state.
Startup time≤2 s
Update rate2000 HzMaximum.
Dimensions64.8 × 47 × 35.3 mm
Weight130 ± 10 g
Temperature range-40 ~ +80 °COperating.
Storage temperature range-55~+85 °CStorage.
Vibration6.06 g20~2000 HZ; RMS.
Shock500 g1ms.

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