Pose and Shape Reconstruction of a Noncooperative Spacecraft Using Camera and Range Measurements

Table 2

Comparison between the norms of the errors at the beginning and at the end of the simulation. The 2-norm has been used for the inertia matrix error calculation.

	Initial errors	Final errors
(m)
(m)
(deg/s)
(m)
(m/s)
(kg m^2)