SNC600D-A0-Beijing Space Navigation and Control Technology Co., Ltd.

SNC600D-A0: Product type：; Views：

Details
Specifications

SNC600D-A0 is an inertial/visual/satellite integrated navigation system that highly integrates visual odometry technology, rotating modulation inertial navigation technology, and array IMU technology, achieving low-cost autonomous navigation under satellite denial. The product can be widely used in composite wing drones, fixed wing drones, and multi-rotor drones.

Physical Dimensions and Electrical Index
Voltage		10-36VDC
Power Consumption		≤10W
Size		≤120mmx104mmx152mm
Weight		≤800g
Environmental Index
Working Temperature		-20℃-65℃（Low temperature can be extended to -40 ℃）
Storage Temperature		-45℃~+70℃
Vibration		5~2000Hz，6.06g
Shock		30g，11ms
Lifetime		>15 years
Continuous Working Time		>24h
Interface Features
RS422
System Performance Index
	Test Conditions		Index
Position Accuracy	GNSS Valid，Single Point		1.2m（RMS）
	GNSS Invalid，Inertial/visual Integrated Navigation Accuracy		5%D（CEP），D is distance
	GNSS and Visual Invalid, Pure Navigation		1km/10min（CEP）
Heading Accuracy	GNSS Valid		0.5°（RMS）
	GNSS Invalid，Inertial/visual Integrated Navigation Accuracy		3°（RMS）
	GNSS and Visual Invalid, Pure Navigation		1°/10min（RMS）
Attitude Accuracy	GNSS Valid		0.5°（RMS）
	GNSS Invalid，Inertial/visual Integrated Navigation Accuracy		1°（RMS）
	GNSS and Visual Invalid, Pure Navigation		1°/10min（RMS）
Velocity Accuracy	GNSS Valid		0.2m/s（RMS）
	GNSS Invalid，Inertial/visual Integrated Navigation Accuracy		0.2m/s（RMS）
	GNSS and Visual Invalid, Pure Navigation		2m/s/10min（RMS）
IMU Performance Index
Gyro	Range		±500°/s
	Bias Stability		≤0.3°/h（10s，RMS）
Accelerometer	Range		±16g
	Bias Stability		≤100μg（10s，RMS）

SNC600D-A0

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