Attitude Determination with Magnetometers and Accelerometers to Use in Satellite Simulator

Table 2

Calibration results of the 3-axis accelerometers: biases and scale factors.

Variable	Values (g)	Standard deviation (g)
Bias N	0.03572	0.00080
Bias E	−0.02001	0.00088
Bias D	−0.00328	0.00008
Scale factor N	1.00000	0.00000
Scale factor E	1.00000	0.00000
Scale factor D	1.00000	0.00000