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MFOG-24 Aerospace Fiber Optic Gyroscope 1.5 deg/h Bias for Satellite Attitude Control Systems

MFOG-24 Aerospace Fiber Optic Gyroscope 1.5 deg/h Bias for Satellite Attitude Control Systems

브랜드 이름: Firepower
모델 번호: MFOG-24
자세한 정보
원래 장소:
중국
인증:
ISO 9001:2015, CE, RoHS
바이어스 안정도:
<=2도/시간
공급 전압:
+5V
최대 각속도:
+/-500도/초
대역폭:
>=300Hz
랜덤 워크 계수:
<=0.04도/rt-h
출력 유형:
비슷한 물건
강조하다:

aerospace fiber optic gyroscope

,

satellite attitude control sensor

,

1.5 deg/h bias aerospace gyro

제품 설명
MFOG-24 Aerospace Fiber Optic Gyroscope 1.5 deg/h Bias for Satellite Attitude Control Systems
Product Overview

The MFOG-24 is an aerospace-grade fiber optic gyroscope configured for satellite attitude determination and control systems (ADCS). Its solid-state construction with radiation-tolerant optical components provides reliable angular rate sensing in the harsh space environment.

Leveraging the Sagnac effect with polarization-maintaining fiber coil, the MFOG-24 achieves 1.5 deg/h bias stability with 0.03 deg/rt-h angular random walk. The vacuum-compatible design and wide operating temperature range make it suitable for LEO satellite missions.

Key Features
  • Radiation-tolerant optical components for LEO space environment
  • Angular rate range: +/-500 deg/s, zero-bias stability <=1.5 deg/h (1 sigma)
  • Angular random walk: <=0.03 deg/rt-h for precise spacecraft pointing
  • Operating temperature: -40 to +65 deg C for satellite thermal conditions
  • No moving parts eliminates lubrication and mechanical failure modes
  • Compact phi24x39mm, 30g minimizes payload mass budget
Technical Specifications
ParameterUnitSpecification
Measurement Rangedeg/s+/-500
Zero-Bias Stability (10s, 1 sigma)deg/h<=2
Zero-Bias Repeatability (1 sigma)deg/h<=2
Angular Random Walkdeg/rt-h<=0.04
Scale Factor Nonlinearityppm300
Bandwidth (3dB)Hz>=300
Output Type--Analog Voltage
Power SupplyV5 +/-0.15
Power ConsumptionW<=1.5
Operating Temperaturedeg C-40 to +65
Storage Temperaturedeg C-55 to +85
Random Vibrationg20, 20-2000 Hz
Dimensionsmmphi24 x 39
Weightg<=30
MTBFh50,000
Applications

Satellite attitude control, spacecraft reaction wheel backup, CubeSat ADCS, launch vehicle guidance, space telescope pointing, orbital maneuvering systems.

Electrical Interface
PinDefinition
15V
2Analog Output Low
3Analog Output High
4GND
15V
2Analog Output Low
3Analog Output High
4GND