Fiber-Optic INS (FOGs + quartz accelerometers)System; BEFGM50A, 60A, 70A, 98A, 120A

The fiber-optic inertial navigation system employs fiber-optic gyroscopes and quartz accelerometers as core sensors, combined with advanced strapdown technology and navigation calculation software, to provide real-time high-precision navigation information. The system supports multiple operation modes such as inertial/satellite navigation integration and inertial autonomous navigation, and is suitable for radar, photoelectric, sonar platforms, as well as robots, vehicles, ships, aircraft, air special aircraft, and high-end industrial equipment. In cases where satellite navigation is restricted or unavailable, the system can still work autonomously, outputting navigation solution data and original inertial device data, without geographical restrictions, and with high reliability.

Series		UMFO-INS   Series
Model		BEFGM50A	BEFGM60A	BEFGM70A	BEFGM98A	BEFGM120A
Accelerometer	Months Bias Repeatability	≤50μg	≤50μg	≤20μg	≤10μg	≤10μg
	Months Scale Factor Accuracy	≤50ppm	≤50ppm	≤20ppm	≤10ppm	≤10ppm
Gyro	Bias Repeatability	0.04°/hr~0.02°/hr	0.02°/hr~0.01°/hr	0.01°/hr~0.005°/hr	0.005°/hr~0.003°/h	0.003°/hr~0.001°/hr
	Scale Factor Accuracy	≤50ppm	≤50ppm	≤20ppm	≤20ppm	≤20ppm
	Random walk	≤0.007°/√hr,1σ	≤0.005°/√hr,1σ	≤0.003°/√hr,1σ	≤0.0008°/√hr,1σ	≤0.0006°/√hr,1σ