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Nonlinear observers for attitude estimation in gyroless spacecraft via Extended Kalman filter algorithm

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Figure

Table 1: RazakSAT’s characteristics. 25.4 kg.m2 26.2 kg.m2
Figure 1: Real measurement of roll angle provided by attitude sensor.
Figure 4: Comparison between the estimated and the real angular velocity around X-axis
Figure 7: Error of estimated angular velocity around X-axis.

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