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. 2018 Apr 18;5:41. doi: 10.3389/frobt.2018.00041

Table 5.

Spatial spacecraft-manipulator system with six-link manipulator: mass and inertia properties (Yoshida and Umetani, 1993).

Link Mass [kg] Length [m] Principal moments-of-inertia [kg m2]
Ixx Iyy Izz
Base-spacecraft 1,700 3.5 1,434 1,434 1,735
1 5 0.5 0.0292 0.0292 0.0063
2 50 2.5 0.0625 26.1000 26.1000
3 50 2.5 0.0625 26.1000 26.1000
4 10 0.5 0.0125 0.2150 0.2150
5 5 0.25 0.0063 0.0292 0.0292
6 5 0.25 0.0063 0.0292 0.0292