Research Article
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 |
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