A Simplified Kalman Filter for Integrated Navigation System with Low-Dynamic Movement

Table 2

Sensor errors in SINS.

Axis	Gyro bias (/h)		Acce. bias (g)
	Constant	Random	Constant	Random
	0.02	0.02	50	50
	0.02	0.02	50	50
	0.02	0.02	50	50