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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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Dynamic Optic Gyroscope Sensor For Inertial Platform Stabilizing
APPLICATIONS:
●UAV/AUV/Helicopter
●Aeronautics and astronautics
●Integrated navigation system
●inertial platform stabilizing
●Vehicle navigation
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
REQUIREMENTS FOR TRANSPORTATION AND STORAGE OF GYRO
Transportation notice
a) Place the product according to the direction shown in the packing box；
b) When the temperature range is -40℃～+70℃, it is allowed to be transported by road, railway, air and water transportation;
c) Ensure that the packing box is fastened to the carrier without moving during shipment.
Storage notice
a) The products placed in the packing box should be stored in an air conditioned warehouse under standard atmospheric pressure,environmental temperature is 15℃～35℃；
b) The storage period of the product is 15 years.
UPPACKING AND INSPECTION
Unpacking inspection
a) Check the appearance of the packing box for collision and other physical damage；
b) Static electricity protection should be carried out when taking out the product .
Inspection of supporting delivery documents
a) Product qualification certificate；
b) F70G Acceptance report of closed loop fiber optic gyroscope；
c) F70G Maintenance instructions for closed-loop fiber optic gyroscope( 1pcs per batch)
DIMENSIONS:
PERFORMANCE CHARACTERISTICS:
| No. | Parameter | F70G | Unit | Remarks | |||||
| 1 | Maximum angular rate | ±800 | °/s | ||||||
| 2 | Scale factor | 45000× (1±5%) | SP/°/s | ||||||
| 3 | Scale factor nonlinearity in room temperature | ≤50 | ppm | @25℃ | |||||
| 4 | Scale factor repeatability in room temperature | ≤50 | ppm | @25℃ | |||||
| 5 | Scale factor repeatability in full temperature
| ≤100 | ppm | -40℃~+70℃ | |||||
| 6 | Bias stability in room temperature | ≤0.1 | 10s(1σ,°/h) | @25℃ | |||||
| 7 | Bias repeatability in room temperature | ≤0.1 | (1σ,°/h) | Bias | |||||
| 8 | Bias repeatability in tull temperature | ≤0.2 | (1σ,°/h) | -40℃~+70℃ | |||||
| 9 | Activation time | 0 | min | ||||||
| 10 | Random Walk | 0.005 | º/√h | ||||||
| 11 | Bias value during vibration/before vibration/ after vibration | ≤0.3 | °/h | ||||||
| 12 | Bias value before/after vibration) | ≤0.3 | °/h | ||||||
| 13 | Magnetic sensitivity | ≤0.2 | °/h/Gs | Optional | |||||
| 14 | Bias stability during Vacuum changing | ≤0.3 | °/h | 0~0.085~0Mpa@2min | |||||
| 15 | Vibration | 20Hz～2000Hz
| Hz/10min | ||||||
| X | Y | Z | |||||||
| 16 | Impact | 15g(3times) | Half sine wave/11ms | ||||||
| ±X | ±Y | ±Z | |||||||
Power Supply
| Power supply | +5V | -5V |
| The fluctuation of voltage | 4.75V~5.25V | -4.75V~-5.25V |
| Rated ripple voltage | 20mV | 20mV |
| Power consumption | 1.5A | 0.6A |
