Error Assessment Model for the Inverse Kinematics Problem for Stewart Parallel Mechanisms for Accurate Aerospace Optical Linkage

Table 1

Total errors of the platform due to manufacture, assembly, backlash, and sensing for optical LEO link application.

Error	Value
(mrad)	1.745
(mrad)	1.747
(mrad)	1.744
(mrad)	1.743
(mrad)	1.746
(mrad)	1.745
(mrad)	1.746
(mrad)	1.748
(mrad)	1.743
(mrad)	1.744
(mrad)	1.747
(mrad)	1.745
(mm)	0.15
(mm)	0.1
(cm)	0.1
(cm)	0.1
(cm)	0.1