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Girocompás del acelerómetro de IMU
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Honeywell HG4930 6-DoF IMU with ±200°/s Gyro and ±30g Accelerometer

Honeywell HG4930 6-DoF IMU with ±200°/s Gyro and ±30g Accelerometer

Nombre De La Marca: FIREPOWER
Número De Modelo: HG4930C
Cuota De Producción: 1
Precio: 6500$
Condiciones De Pago: L/C, D/P, T/T, Western Union
Capacidad De Suministro: 1 semana para la muestra
Información detallada
Lugar de origen:
PORCELANA
Certificación:
CE
Rango de medición girodinámico:
± 200 °/s (personalizable)
Estabilidad de sesgo cero (@ Allan variance):
≤ 0,2 °/h
Estabilidad de sesgo cero ((10s suave):
≤0.5 °/h
Paseo al azar:
0.02°/√h
Ancho de banda:
100Hz
Rango de acc:
±30g
Acc Estabilidad de sesgo cero (varianza de Allan):
30g
Voltaje:
5V
Vibración:
10 ~ 2000Hz , 6.06g
Peso:
120 g
Detalles de empaquetado:
Esponja + cartón
Capacidad de la fuente:
1 semana para la muestra
Resaltar:

Honeywell HG4930 IMU sensor

,

6-DoF IMU with gyro

,

IMU accelerometer with warranty

Descripción del Producto
Honeywell HG4930 6-DoF Inertial Measurement Unit with Integrated Gyroscope and Accelerometer

The Honeywell HG4930 is a tactical grade MEMS Inertial Measurement Unit replacement designed for high-performance applications. This compact and rugged navigation sensor is engineered for demanding environments across aerospace, defense, UAVs, robotics, marine, and industrial automation sectors.

Key Features
  • Integrated three-axis gyroscope and three-axis accelerometer
  • Built-in temperature sensor for environmental compensation
  • Advanced signal processing board for real-time motion data
  • Durable mechanical structure for harsh environments
  • Precise measurement of angular rate, linear acceleration, and inclination angles
  • Temperature correction and installation misalignment compensation
  • Nonlinear behavior correction for stable, accurate information
  • Reliable performance under high dynamics and extreme conditions
Gyroscope Specifications
Parameter Unit HG4930C
Measuring range (customizable) °/s ±200
Zero-bias stability (@ Allan variance) °/h 0.2
Zero-bias stability (10 s smoothing, 1σ, room temperature) °/h 0.5
Zero-bias error over full temperature range °/h 2.5
Random walk °/√h 0.02
Zero-bias repeatability °/h 1
Zero bias acceleration sensitivity °/h/g 1
Resolution °/h 2
Scale factor nonlinearity ppm 100
Scale factor repeatability ppm 100
Cross coupling % 0.2
Bandwidth Hz 100
Accelerometer Specifications
Parameter Unit HG4930C
Measuring range (customizable) g ±30
Zero-bias stability (Allan Variance @ 25 ℃) ug 30
Zero-bias stability (1s smoothing) ug 700
Zero-bias error over full temperature range mg 1.5
Random walk m/s/√h 0.01
Zero-bias repeatability mg 2
Scale factor repeatability ppm 200
Scale factor nonlinearity ppm 200
Cross coupling % 0.2
Bandwidth Hz 100
Outline Drawing
Honeywell HG4930 6-DoF IMU with ±200°/s Gyro and ±30g Accelerometer 0