항공기 천체 항법용 5V 전원 공급 파이버 광 자이로 자이로

• Type: Servo
• Output Signal Type: Digital Output
• Measuring Shaft Quantities: Single
• Accuracy Grade: ≤0.05°/H
• IP Rating: IP67
• Certification: CE
• 모델 번호.: F60
• Customized: Customized
• 비선형성 축척 계수: 50ppm 미만(1sigma;)
• 척도 계수 비대칭: 50ppm 미만
• 축척 계수 반복성: 50ppm 미만
• 다이나믹 레인지: 300도;/초
• 제로 바이어스 안정성: 0.05 도, /h(1sigma;) 미만
• 대역폭: >200Hz
• 운송 패키지: Sponge and Box
• 사양: 70mm× 70mm× 32mm
• 세관코드: 9031809090
• 생산 능력: 500/Month

제품 설명

5v Power Supply Fiber Optic Gyro for Aircraft Inertial Navigation Gyro

Fiber optic gyroscope is a kind of fiber sensor sensitive to angular rate. Its basic working principle is to use the Sagnac effect: In a ring interferometer, the light wave emitted by the light source is divided into two by the beam splitter, and the two beams of light will be along the forward and backward directions respectively. Move counterclockwise and return to the beam splitter

Product structure and features
The gyroscope structure adopts a typical optical fiber ring structure design scheme, and from the miniaturization integrated design, structural stability (resistance to shock and vibration), anti-resonance, structural symmetry, ease of installation and thermal design (temperature Characteristics) and other aspects were considered, and the existing structure of the gyro was optimized and designed.

main gyro parameters
Non-linearity scale factor: ≤50ppm (1σ)
Scale factor asymmetry: ≤50ppm (1σ)
Scale factor repeatability: ≤50ppm (1σ)
Dynamic range: ±300°/s
Zero bias stability: ≤0.05°/h (1σ)
Zero bias repeatability: ≤0.05°/h (1σ)
Random walk coefficient: ≤0.005°/√h
Bandwidth: ≥200Hz
Weight: ≤250g

Interface

Node number	Definition	Remark
1	+5V	+5V power input
2	+5V	+5V power input
3	-5V	-5V power input
4	-5V	-5V power input
5	±5VGND	Power ground (Note: must not be connected to the gyro shell)
6	±5VGND	Power ground (Note: must not be connected to the gyro shell)
7	T+	Gyro output signal+
18	T-	Gyro output signal-
the remaining	Disable

Comany and production