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MFOG-910 Navigation Grade Fiber Optic Gyroscope with 0.8 deg/h Bias Stability 1000Hz Bandwidth and 70g Vibration Resistance

MFOG-910 Navigation Grade Fiber Optic Gyroscope with 0.8 deg/h Bias Stability 1000Hz Bandwidth and 70g Vibration Resistance

ब्रांड नाम: FIREPOWER
मॉडल संख्या: MFOG-910
विस्तृत जानकारी
उत्पत्ति के प्लेस:
चीन
प्रमाणन:
ISO 9001:2015, CE, RoHS
शून्य-पूर्वाग्रह स्थिरता:
0.8 डिग्री/घंटा
पूर्वाग्रह पुनरावृत्ति:
0.8 डिग्री/घंटा
माप श्रेणी:
240 डिग्री/से
स्केल फ़ैक्टर गैर-रैखिकता:
<=1000 पीपीएम
आकार:
82 मिमी x 82 मिमी x 19.5 मिमी
त्वरण:
>=70 ग्राम
प्रमुखता देना:

navigation grade fiber optic gyroscope

,

aerospace inertial navigation FOG sensor

,

0.8 deg/h bias MFOG-910 gyro

उत्पाद वर्णन
MFOG-910 Navigation Grade Fiber Optic Gyroscope 0.8 deg/h Bias Aerospace Inertial Navigation Sensor
Product Overview

The MFOG-910 is a navigation-grade fiber optic gyroscope integrating optical, mechanical, and electronic technologies in a compact 82mm×82mm×19.5mm package. Utilizing the Sagnac effect with micro-nano fiber-optic devices, it delivers precise 0.8 deg/h bias stability for demanding aerospace inertial navigation systems.

Engineered with no moving or wearing components, the MFOG-910 ensures rapid startup, exceptional reliability, and consistent performance across wide temperature ranges. Its 1000Hz bandwidth and 0.02 deg/rt-h random walk make it the preferred choice for flight control computers and navigation-grade IMU integration.

Technical Specifications
Parameter Specification
Range (deg/s) +/-240
Scale Factor (mV/deg/s) 47+/-5
Scale Factor Nonlinearity (ppm) <=1000
Zero-Bias Stability (10s, 1 sigma, deg/H) <=0.8
Zero-Bias Repeatability (1 sigma, deg/H) <=0.8
3dB Bandwidth (Hz) >=1000
Random Walk (deg/rt-H) <=0.02
Power Supply (V) 5+/-0.25+12
Power Consumption (W) <=1.5
Impact Resistance (g) >=1500
Vibration Resistance (g) >=70
Service Life (years) >=15
MTBF (Calculated) >=100,000 hours
Key Features
  • Navigation-grade 0.8 deg/h bias stability for precision INS
  • High 1000Hz bandwidth for dynamic flight maneuver sensing
  • Ultra-low 0.02 deg/rt-h angular random walk
  • Solid-state micro-nano design with no moving parts
  • 1500g impact and 70g vibration resistance
  • 100,000+ hour MTBF with 15-year service life
Applications
  • Aerospace inertial navigation systems
  • Flight control computers
  • Navigation-grade IMU integration
  • Launch vehicle guidance
  • Spacecraft attitude determination
  • High-altitude UAV autopilot