logo

Chi tiết sản phẩm

Created with Pixso. Trang chủ Created with Pixso. các sản phẩm Created with Pixso.
Con quay gia tốc kế IMU
Created with Pixso.

High-Performance Inertial Measurement Unit for Inertial Navigation System INS

High-Performance Inertial Measurement Unit for Inertial Navigation System INS

Tên thương hiệu: FIREPOWER
Số mẫu: IMU6-36
MOQ: 1
Điều khoản thanh toán: L/C,T/T
Khả năng cung cấp: 500/tháng
Thông tin chi tiết
Nguồn gốc:
Trung Quốc
Sự bất ổn không thiên vị:
≤3 °/h
Phạm vi đo:
480°/giây
Bước đi ngẫu nhiên góc:
0,25°/√ giờ
Phạm vi đo (Gia tốc kế):
Cấu hình 2 ~ 16g
Độ lặp lại không sai lệch:
5°/giờ
Băng thông:
≥100Hz
Cân nặng:
18g
Điện áp:
5±0.3V
chi tiết đóng gói:
miếng bọt biển + thùng carton
Khả năng cung cấp:
500/tháng
Làm nổi bật:

Inertial Measurement Unit for navigation

,

High-performance INS accelerometer

,

Gyro sensor for inertial systems

Mô tả sản phẩm
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