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مقياس تسارع IMU الدوران
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Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

اسم العلامة التجارية: FIREPOWER
رقم الطراز: 16488HB
الـ MOQ: 1
شروط الدفع: الاعتماد المستندي، تي/تي
القدرة على التوريد: 500/شهر
معلومات مفصلة
مكان المنشأ:
الصين
نطاق القياس الديناميكي:
± 2000 درجة/ثانية
عدم الاستقرار التحيز:
3 درجة/ساعة
المشي العشوائي الزاوي:
0.15 درجة/ √ ساعة
دقة معامل القياس، المحور Z:
0.3 ٪
عرض النطاق الترددي:
200 هرتز
واجهة الاتصالات:
سبي/كان
تفاصيل التغليف:
الاسفنج + الكرتون
القدرة على العرض:
500/شهر
إبراز:

Adis16488 IMU with magnetometer,UAV stabilization IMU sensor,drone gyro accelerometer system

,

UAV stabilization IMU sensor

,

drone gyro accelerometer system

وصف المنتج
ADIS16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer

The ADIS16488HB multi-degree-of-freedom inertial measurement unit is a complete inertial system featuring a three-axis gyroscope, three-axis accelerometer, three-axis magnetometer, and pressure sensor. This advanced IMU measures three-axis angular rate, acceleration, three-axis magnetic field, air pressure, and other critical parameters. The unit outputs error-compensated data (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) through SPI or UART communication protocols.

Technical Specifications
ParameterTest conditionsMinimum valueTypical valueMaximum valueUnit
GyroscopeDynamic measuring range5002000°/s
Zero bias stabilityAllan variance, Z-axis0.8°/h
Allan variance, X and Y axis1.6°/h
10 s average (-40 ℃ ~ + 70 ℃, constant temperature),
Z-axis
3°/h
10 s average (-40 ℃ ~ + 70 ℃, constant temperature),
X-axis and Y-axis
6°/h
Zero biasZero-bias range, Z-axis±0.07°/s
Zero-bias range, X-axis and Y-axis±0.2°/s
Zero-bias change in full temperature range, Z-axis ①±0.02°/s
Zero Bias Change Over Temperature, X and Y
Axis ①
±0.06°/s
Successive Start Repeatability, Z-axis0.002
Successive Start Repeatability, X-Axis and Y-Axis0.006
Day-by-day start repeatability, Z-axis0.003/s
Start repetition day by day, X axis and Y axis0.009°/s
Ffect of linear acceleration on bias0.002°/s/g
Influence of vibration on zero bias, change before and after vibration ②0.002°/s/g
Influence of vibration on zero bias, change before and during vibration ②0.002°/s/g
Scale factorScale factor accuracy, Z-axis0.3%
Scale Factor Accuracy, X and Y Axis0.6%
Scale factor nonlinearity, Z-axis0.01%FS
Scale Factor Nonlinearity, X and Y Axis0.02%FS
Angular random walk0.15°/ √hr
Noise density0.001°/s/ √Hz
Resolution3.052*10-7/s/LSB
Bandwidth200Hz
AccelerometerDynamic measuring range16200g
Zero bias stabilityAllan variance0.06mg
10 s average (-40 ℃ ~ + 70 ℃, constant temperature)0.4mg
Zero biasZero bias range2mg
Change of zero bias within the whole temperature range, peak-to-peak value ①4mg
Repeatability of successive starts0.5mg
Repeatability is initiated on a daily basis0.8mg
Zero-bias temperature coefficient0.050.1mg/℃
MagnetometerMagnetic field rangeBrg,xy±13gauss
Brg,z±25gauss
Resolution0.3μT
Heading accuracy30 μT horizontal geomagnetic component, 25 ℃±2.5deg
Dynamic measuring range2.5gauss
Zero biasNon-magnetic environment15mgausS
BarometerDynamic measuring range3001100mbar
Zero bias4.5mbar
Communication interface1-way SPIBaud rate15MHz
1-Way C A NBaud rate1MHz
Sampling frequencySPI24602460Hz
CAN200
Electrical characteristicsVoltage3.03.33.6V
Power consumption1.5W
RippleP-P100mV
Settling timeFrom 0 V to 3. 3V80ms
Structural characteristicsSize47*44*14mm
Weight50g
Use environmentOperating temperature-4070
Storage temperature-4575
ReliabilityMTBF20000h
Continuous working time120h

①: Calculate the zero deviation of the whole temperature change process, the temperature change rate is ≤ 1 ℃/min, and the temperature range is -40 ℃ ~ + 70 ℃
②: Vibration condition is 6.06 G, 20Hz ~ 2000Hz

Table 1. 16488HB Product Index

Outline Drawing
Adis16488 Inertial Sensor IMU for UAV and Drone Stabilization System with Magnetometer 0