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Girobussola dell'accelerometro di IMU
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HG4930C Inertial Sensor 200°/s Gyro 30g Acc for Unmanned Vehicles

HG4930C Inertial Sensor 200°/s Gyro 30g Acc for Unmanned Vehicles

Marchio: FIREPOWER
Numero di modello: HG4930C
MOQ: 1
prezzo: 6500$
Condizioni di pagamento: L/C, D/P, T/T, Western Union
Capacità di approvvigionamento: 1 settimana per il campione
Informazioni dettagliate
Luogo di origine:
Cina
Certificazione:
CE
Distanza di misura girodinamica:
± 200 °/s (personalizzabile)
Stabilità a pregiudizio zero (@ Allan variance):
≤ 0,2 °/h
Stabilità di sbiadimento zero ((10s liscia):
≤0,5 °/h
Passeggiata casuale:
00,02°/√h
Larghezza di banda:
100Hz
Intervallo di acc:
±30 g
Acc Stabilità a bias zero (varianza di Allan):
30ug
Voltaggio:
5v
Vibrazione:
10 ~ 2000Hz , 6,06G
Peso:
120g
Imballaggi particolari:
Sponge + Carton
Capacità di alimentazione:
1 settimana per il campione
Evidenziare:

IMU sensor for unmanned vehicles

,

200°/s gyro inertial sensor

,

30g accelerometer gyro sensor

Descrizione del prodotto
Precision Guidance HG4930C Inertial Sensor for Unmanned Vehicle
Tactical Grade MEMS Inertial Measurement Unit Honeywell HG4930 Replacement. The MEMS Inertial Measurement Unit (IMU) consists of three-axis gyroscope, three-axis accelerometer, temperature sensor, signal processing board, structure and necessary software. It measures three-axis angular rate, three-axis acceleration and three-axis inclination angle of a carrier, outputting compensated data (including temperature compensation, installation misalignment angle compensation, and nonlinear compensation) through RS-422 serial port using an agreed communication protocol.
Technical Specifications
Gyroscope Specification
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 Specification
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
HG4930C Inertial Sensor 200°/s Gyro 30g Acc for Unmanned Vehicles 0
Honeywell HG4930 Inertial Measurement Unit outline drawing