International Journal of Aerospace Engineering / 2019 / Article / Tab 4

Research Article

Pose Determination for Malfunctioned Satellites Based on Depth Information

Table 4

The eigenvalues.

Error (cm)Eigenvalues (simulation)Eigenvalues (theory)

0(8.5595, 26.7923, 0)(8.3333, 27, 0)
0.01(8.5898, 26.9769, 0.0001)(8,3334, 27.0001, 0.0001)
0.1(8.3124, 26.9526, 0.0103)(8.3433, 27.01, 0.01)
1(9.4664, 27.7494, 0.9765)(9.3333, 28, 1)

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