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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

ব্র্যান্ড নাম: FIREPOWER
মডেল নম্বর: এমএফওজি -910
বিস্তারিত তথ্য
উৎপত্তি স্থল:
চীন
সাক্ষ্যদান:
ISO 9001:2015, CE, RoHS
জিরো-বায়াস স্থায়িত্ব:
0.8 ডিগ্রী/ঘণ্টা
পক্ষপাত পুনরাবৃত্তিযোগ্যতা:
0.8 ডিগ্রী/ঘণ্টা
পরিমাপ পরিসীমা:
240 ডিগ্রী/সেকেন্ড
স্কেল ফ্যাক্টর অরৈখিকতা:
<=1000 পিপিএম
আকার:
82 মিমি x 82 মিমি x 19.5 মিমি
ত্বরণ:
>=70 গ্রাম
বিশেষভাবে তুলে ধরা:

navigation grade fiber optic gyroscope

,

aerospace inertial navigation FOG sensor

,

0.8 deg/h bias MFOG-910 gyro

পণ্যের বিবরণ
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