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IMU İvmeölçer Gyro
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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

Marka Adı: FIREPOWER
Model Numarası: HG4930C
Moq: 1
fiyat: 6500$
Ödeme Şartları: L/C, D/P, T/T, Western Union
Tedarik Yeteneği: Örnek için 1 hafta
Ayrıntılı Bilgiler
Menşe yeri:
Çin
Sertifika:
CE
Gyro dinamik ölçüm aralığı:
± 200 °/s (özelleştirilebilir)
Sıfır önyargı stabilitesi (@ allan varyansı):
≤0.2 °/s
Sıfır önyargı stabilitesi (10s pürüzsüz):
≤0.5 °/s
Rastgele yürüyüş:
0,02°/√sa
Bant genişliği:
100hz
Acc Aralığı:
±30g
ACC Sıfır Önyargı İstikrarı (Allan Varyansı):
30g
Gerilim:
5V
Titreşim:
10 ~ 2000Hz , 6.06g
Ağırlık:
120g
Ambalaj bilgileri:
Sünger + karton
Yetenek temini:
Örnek için 1 hafta
Vurgulamak:

IMU sensor for unmanned vehicles

,

200°/s gyro inertial sensor

,

30g accelerometer gyro sensor

Ürün Açıklaması
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