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Giroscópio do acelerômetro de 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

Nome da marca: FIREPOWER
Número do modelo: HG4930C
MOQ: 1
preço: 6500$
Condições de pagamento: L/C, D/P, T/T, Western Union
Capacidade de abastecimento: 1 semana para a amostra
Informações pormenorizadas
Lugar de origem:
CHINA
Certificação:
CE
Distância de medição girodinâmica:
± 200 °/s (personalizável)
Estabilidade de viés zero (@ Allan variance):
≤ 0,2 °/h
Estabilidade de desvio zero (< 10s suave):
≤0,5 °/h
Caminhada aleatória:
00,02°/√h
Largura de banda:
100Hz
Faixa de aceleração:
±30g
Acc Estabilidade de desvio zero (variância de Allan):
30g
Tensão:
5V
Vibração:
10 ~ 2000Hz , 6,06g
Peso:
120g
Detalhes da embalagem:
Esponja + Carton
Habilidade da fonte:
1 semana para a amostra
Destacar:

IMU sensor for unmanned vehicles

,

200°/s gyro inertial sensor

,

30g accelerometer gyro sensor

Descrição do produto
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