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[China]
Trade Verify
Address: 803, Block A, Building B5-1, Junfeng Industrial Complex, HepingCommunity, Fuhai Street, Bao an District, Shenzhen
Contact name:Caine
Shenzhen Avionics Technology Co.,Ltd |
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Verified Suppliers
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1 axis FOG low drift inertial gyro navigation gyro sensor
Performance Characteristics
| No. | Parameter | F98-400 | Unit | Remarks | ||||||
| 1 | Maximum angular rate | ±400 | °/s | |||||||
| 2 | Scale factor | 1650000× (1±10%) | SP/°/s | |||||||
| 3 | Scale factor nonlinearity in room temperature | ≤20 | ppm | @25℃ | ||||||
| 4 | Scale factor repeatability in room temperature | ≤20 | ppm | @25℃ | ||||||
| 5 | Scale factor repeatability in full temperature
| ≤50 | ppm | -40℃~+70℃ | ||||||
| 6 | Bias stability in room temperature | ≤0.02 | 10s 1σ,°/h | @25℃ | ||||||
| 7 | Bias repeatability in room temperature | ≤0.01 | 1σ,°/h | Bias | ||||||
| 8 | Bias repeatability in tull temperature | ≤0.03 | 1σ,°/h | -40℃~+70℃ | ||||||
| 9 | Bias stability in changing temperature | ≤0.015 | 100s 1σ,°/h | 0.3℃/min,-40℃~+70℃ | ||||||
| 10 | Random walk | ≤0.003 | °/ | |||||||
| 11 | Activation time | 0 | min | |||||||
| 12 | Bias value during vibration/before vibration/after vibration | ≤0.05 | °/h | |||||||
| 13 | Bias value before/after vibration) | ≤0.05 | °/h | |||||||
| 14 | Magnetic sensitivity | ≤0.01 | °/h/Gs | |||||||
| 15 | Threshold value | ≤0.02 | °/h | |||||||
| 16 | Vibration | 20Hz～2000Hz
| Hz/10min | |||||||
| X | Y | Z | ||||||||
Vibration spectrum | ||||||||||
| 17 | Impact | 15g(3times) | Half sine wave/11ms | |||||||
| ±X | ±Y | ±Z | ||||||||
Dimensions
Features
● All-fiber design -long lifespan, small package size, high stability and more resistance to interference.
● Integrated fiber polarizer -minimum insertion loss and high extinction ratio, offering more resistance to temperature and mechanical shock, as well as intense vibration.
● Reliable compact package -operationally robust for all kinds of environments, ideal for a wide of applications in both civilian and military areas.
● QuichLaunch technology -minium activation time with no external calibration required.
● Optimal wavelength -improves the sensibility by 50% with the same structure, size and cost.
● Noise isolation and compression -significantly reduces the angle random walk.
● SelfTrack technology -improves the gyro dynamic range
Applications
●UAV/AUV/Helicopter ●Tactical nuclear weapons ●Aeronautics and astronautics
●Integrated navigation system ●inertial platform stabilizing ●Vehicle navigation
