Table 2 Controller parameters.

From: Nonlinear adaptive pose motion control of a servicer spacecraft in approximation with an accelerated tumbling target

Attitude motion controller:

\({D}_{x}={D}_{y}={D}_{z}=0.5\)

\({\varepsilon }_{x}={\varepsilon }_{y}={\varepsilon }_{z}=0.05\)

\({d}_{x}={d}_{y}={d}_{z}=0.5\)

\({\lambda }_{0}=3\)

Translational motion controller:

\({D}_{xx}={D}_{yy}={D}_{zz}=50\)

\({\varepsilon }_{xx}={\varepsilon }_{yy}={\varepsilon }_{zz}=0.05\)

\({d}_{xx}={d}_{yy}={d}_{zz}=2,\)

\({\lambda }_{0}=0.1\)

* The initial amount of all the parameters (for adaptation laws) is assumed to be zero

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