Satellites and subsystems > Attitude > Attitude sensors > Gyroscopes > 3-Axis FOG/IRU for microsatellite
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3-AXIS Fiber Optical Gyro(FOG)unit for micro-satellite. The unit is an inertial sensor with electronics and in-house developed optical fiber gyro packaged into a compact unit ideal for 30 to 100kg spacecraft.
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Last updated: 2020-06-11
3-Axis FOG/IRU for microsatellite
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