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مقياس تسارع IMU الدوران
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High-Performance Inertial Measurement Unit for Inertial Navigation System INS

High-Performance Inertial Measurement Unit for Inertial Navigation System INS

اسم العلامة التجارية: FIREPOWER
رقم الطراز: IMU6-36
الـ MOQ: 1
شروط الدفع: الاعتماد المستندي، تي/تي
القدرة على التوريد: 500/شهر
معلومات مفصلة
مكان المنشأ:
الصين
صفر التحيز عدم الاستقرار:
≤3 °/h
نطاق القياس:
480 درجة/ثانية
زاوية المشي العشوائي:
0.25°/√ ح
نطاق القياس (مقياس التسارع):
شكلي 2 ~ 16 جرام
تكرار التحيز الصفري:
≥5°/ساعة
عرض النطاق الترددي:
≥ 100 هرتز
وزن:
18 جرام
الجهد االكهربى:
5 ± 0.3 فولت
تفاصيل التغليف:
الاسفنج + الكرتون
القدرة على العرض:
500/شهر
إبراز:

Inertial Measurement Unit for navigation,High-performance INS accelerometer,Gyro sensor for inertial systems

,

High-performance INS accelerometer

,

Gyro sensor for inertial systems

وصف المنتج
High-Performance Inertial Measurement Unit for Inertial Navigation System INS

Composition and Function
The inertial measurement unit consists of a three-axis gyroscope, three-axis accelerometer, temperature sensor, signal processing board, structural components, and essential software. It measures the three-axis angular rate and acceleration of the carrier, outputting compensated data including temperature compensation, installation misalignment angle compensation, and nonlinear compensation through the UART serial port using the specified communication protocol.

Gyroscope Technical Specifications
Parameter Unit Test Conditions IMU6-36
Measuring range °/s Configurable ±480
Zero-bias instability °/h Allan variance ≤3
Zero bias stability °/h 10s smooth, RMS, normal temperature ≤8
Zero bias variation at full temperature °/h 10 s smoothing, three-temperature zero-bias variation (-45 ℃, 25 ℃, 85 ℃) ≤150
Random walk °/√h Allan variance ≤0.25
Zero-bias repeatability °/h Q = 6, normal temperature ≤5
Scale factor nonlinearity ppm Normal temperature ≤50
Cross coupling % Normal temperature ≤0.1
Bandwidth Hz Configurable ≥100
Accelerometer Technical Specifications
Parameter Unit Test Conditions IMU6-36
Measuring range g Configurable 2 ~ 16g ±16
Zero bias stability mg 10s smooth, RMS, normal temperature ≤0.1
Zero bias variation at full temperature mg 10 s smoothing, three-temperature zero-bias variation (-45 ℃, 25 ℃, 85 ℃) ≤2.5
Zero-bias repeatability mg Q = 6, normal temperature ≤0.1
Scale factor nonlinearity ppm Normal temperature, ± 1 g ≤200
Cross coupling % Normal temperature ≤0.1
Bandwidth Hz Configurable ≥100
Power Supply Requirements
Parameter Unit IMU6-36
Voltage V 5±0.3
Starting current mA 100
Steady-state power consumption W ≤0.25
Ripple mV 100
Environmental Adaptability
Parameter Unit IMU6-36
Operating temperature -45~85
Storage temperature -55~105
Additional Specifications
Parameter Unit IMU6-36
Weight g 18±1
Start time s ≤2
Outline Drawing
High-Performance Inertial Measurement Unit for Inertial Navigation System INS 0