SD701

SD701 MEMS Integrated Inertial Navigation System

The product is composed of high-precision MEMS gyroscope and accelerometer. The main features of the product are as follows:

a) Full navigation parameter output: carrier angular rate, attitude angle, speed, position, etc.;
b) Integrated navigation function: can be combined with external GPS/BD receiver information, geomagnetic information, etc.

SD701 MEMS Integrated Inertial Navigation System

Suitable for the field of attitude measurement and navigation of drones.

	Parameter	Technical specification
System Specifications	Position accuracy	< 10m (1σ)
	Heading accuracy (180s)	≤2°
	Horizontal attitude accuracy	≤2°
	Start Time	2s
Fiber Optic Gyro Specifications	Zero bias stability (1σ, 100s)	30°/h
	Scale factor repeatability (1σ)	0.1%
	Measuring range	±400°/s
Accelerometer Specifications	Zero bias stability (1σ, 100s)	2mg
	Scale factor repeatability (1σ)	0.3%
	Measuring range	±18 g
Physical Specifications	volume	96mm×96mm×50mm
	weight	≤ 0.35kg
	Maximum power consumption	≤ 5W
	Operating temperature	-40 ℃ ~ 65 ℃
	Electrical Interface	RS422
	Power supply requirements	18 ~ 36 VDC

SD701