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AMU30
The second of a family of High Performance IMUs (HPIMUs), AMU30 is another ground-breaking, non-ITAR, MEMS IMU alternative to more costly ‘FOG-grade’ IMUs, which also includes a 3-axis magnetometer, pressure sensor and sophisticated AHRS algorithm.
Available for customer evaluation, the AMU30 is proving a formidable choice for affordable high-performance IMUs, where users also benefit from the availability of roll. pitch and heading angle outputs. It is ideally suited to the survey market, as well as Inertial Navigation Systems (INS) and autonomous guidance and control.
Product Lifecycle Status
Production Status: Pre-production
Availability: Sampling
Customer Applications: New and existing applications
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- Axes of Acceleration
- Axes of Angular Rate
- Roll/Pitch Error
- Heading Error (Magnetic)
- Altitude
- Altitude Output
- Supply Voltage (Vdd)
- Dynamic Range
- Bias Instability
- Bias over Temperature
- Operating Temperature
- Current Consumption
- Dimensions (mm)
- Mounting Options
- Interface
- Baud Rate
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AMU30-02
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Axes of Acceleration : 3
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Axes of Angular Rate : 3
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Roll/Pitch Error : ±0.1°
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Heading Error (Magnetic) : ±1.0°
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Altitude : 0-60,000ft
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Altitude Output : <=1m
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Supply Voltage (Vdd) : 4.75V to 36V
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Dynamic Range : ±490°/s, ±10g
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Bias Instability : 0.1°/hr, 0.015mg
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Bias over Temperature : ±15°/hr, ±1.5mg
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Operating Temperature : -40°C to +85°C
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Current Consumption : 250mA (at 12V)
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Dimensions (mm) : 68.5 x 61.5 x 65.5
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Mounting Options : Sealed Case
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Interface : RS422
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Baud Rate : 460,800 baud
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Product description
The second of a family of High Performance IMUs (HPIMUs), AMU30 is another ground-breaking, non-ITAR, MEMS IMU alternative to more costly ‘FOG-grade’ IMUs, which also includes a 3-axis magnetometer, pressure sensor and sophisticated AHRS algorithm.
Available for customer evaluation, the AMU30 is proving a formidable choice for affordable high-performance IMUs, where users also benefit from the availability of roll. pitch and heading angle outputs. It is ideally suited to the survey market, as well as Inertial Navigation Systems (INS) and autonomous guidance and control.
