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10 Axis High Precision IMU with Gyro Accelerometer Magnetometer & Barometer

10 Axis High Precision IMU with Gyro Accelerometer Magnetometer & Barometer

نام تجاری: Firepower
شماره مدل: 16488HB
مقدار تولیدی: 1
شرایط پرداخت: L/C، T/T
توانایی عرضه: 500/ماه
اطلاعات دقیق
محل منبع:
چین
محدوده اندازه گیری:
500/2000 درجه در ثانیه
ثبات بایاس صفر:
0.8 درجه در ساعت
پهنای باند:
200 هرتز
ضریب راه رفتن تصادفی:
≤0.15 درجه در ساعت
تغییر سوگیری صفر بر روی دما، محور X و Y:
± 0.06 درجه در ثانیه
تراکم سر و صدا:
0.001°/s/ √Hz
جزئیات بسته بندی:
اسفنج + کارتن
قابلیت ارائه:
500/ماه
برجسته کردن:

10 axis high precision IMU,IMU with gyro accelerometer,high precision magnetometer barometer

,

IMU with gyro accelerometer

,

high precision magnetometer barometer

توضیح محصول
10 Axis High Precision IMU with Gyro, Accelerometer, Magnetometer & Barometer
Product Overview

The 16488HB Inertial Measurement Unit (IMU) is a high-performance MEMS-based IMU featuring a three-axis digital gyroscope, accelerometer, and magnetometer. This precision navigation unit offers a dynamic range of ±2000º/s for the gyroscope and ±200g for the accelerometer. With exceptional reliability and environmental adaptability, it's an ideal solution for unmanned motion carriers, mobile communication, and surveying applications. This model serves as a complete replacement for the Adis 16497, providing enhanced accuracy and stability for critical operations.

Product Features
  • Three-axis digital gyroscope: ±2000º/s dynamic measurement range with zero bias stability of 3°/H (GJB, 10S, Z-axis) and 0.8°/H (ALLAN, Z-axis)
  • Triaxial digital accelerometer: ±200g dynamic measurement range with zero bias stability of 0.4mg (GJB, 10S) and 0.06mg (ALLAN)
  • Triaxial digital magnetometer: 2.5 gauss measurement range
  • Digital barometer: 300mbar to 1100mbar range
  • High reliability: MTBF 20,000 hours
  • Full temperature range accuracy: Guaranteed performance from -40℃ to +80℃ with built-in temperature calibration and compensation
  • Vibration resistance: Suitable for operation under strong vibration (6.06 G, 20-2000 Hz)
  • Impact resistance: Suitable for working under large impact conditions (1000 G, 0.5ms)
Technical Specifications
Parameter Test Conditions Min Value Typical Value Max Value Unit
Gyroscope
Dynamic measuring range
500
2000 °/s
Zero bias stability Allan variance, Z-axis
0.8
°/h
Zero bias stability Allan variance, X and Y axis
1.6
°/h
Zero bias stability 10s average (-40℃~+70℃, constant temperature), Z-axis
3
°/h
Zero bias stability 10s average (-40℃~+70℃, constant temperature), X and Y axis
6
°/h
Zero bias Zero-bias range, Z-axis
±0.07
°/s
Zero bias Zero-bias range, X and Y axis
±0.2
°/s
Zero bias change in full temperature range Z-axis
±0.02
°/s
Zero bias change over temperature X and Y axis
±0.06
°/s
Scale factor accuracy Z-axis
0.3
%
Scale factor accuracy X and Y axis
0.6
%
Angular random walk

0.15
°/√hr
Noise density

0.001
°/s/√Hz
Accelerometer
Dynamic measuring range
16
200 g
Zero bias stability Allan variance
0.06
mg
Zero bias stability 10s average (-40℃~+70℃, constant temperature)
0.4
mg
Zero bias range

2
mg
Scale factor accuracy

0.5
%
Noise density

0.025
mg/√Hz
Magnetometer
Magnetic field range Brg,xy
±13
gauss
Heading accuracy 30 μT horizontal geomagnetic component, 25℃
±2.5
deg
Electrical Characteristics
Voltage
3.0 3.3 3.6 V
Power consumption

1.5
W
Structural Characteristics
Size

47*44*14
mm
Weight

50
g
Note: Zero bias calculations for full temperature change process assume temperature change rate ≤ 1℃/min within -40℃ to +70℃ range. Vibration conditions are 6.06 G, 20Hz-2000Hz.
Outline Drawing
10 Axis High Precision IMU with Gyro  Accelerometer Magnetometer & Barometer 0