Research Article
Dual Arm Free Flying Space Robot Trajectory Planning Using Polynomial
Table 2
Parameters used in simulating of space robot.
| Mass of base () | 4 kg | Mass of first link of mission and balance arm | 0.2942 kg | Mass of second link of mission and balance arm including masses of their grippers | 0.2942 kg | Length of first link of mission and balance arm | 0.4 m | Length of second link of mission and balance arm | 0.3 m | Distance of CM of base to first joint of both the arms | 0.5 m | Inertia of first link of mission and balance arm | 0.03 kg m2 | Inertia of second link of mission and balance arm including end effectors inertia | 0.02 kg m2 | Inertia of base () | 0.4 kg m2 |
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