In-Flight Self-Alignment Method Aided by Geomagnetism for Moving Basement of Guided Munitions

Table 1

Attitude error by fast coarse method.

Time (s)	(rad)	(rad)	(rad)
0.43	0.017	0.008	0.062
0.77	−0.008	0.0014	0.051
1.09	−0.014	0.009	−0.074
2.81	0.09	0.0041	0.081
3.29	0.013	−0.016	0.054
4.33	−0.016	−0.009	−0.063
4.67	0.026	0.012	0.049