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Table 1 The parameters regarding the proposed control strategy

From: High-precision full quaternion based finite-time cascade attitude control strategy considering a class of overactuated space systems

  The parameters The values
1 Space system moments of inertia \( \left\{ {\begin{array}{*{20}c} {I_{x} = 15.95} \\ {I_{y} = 72.19} \\ {I_{z} = 72.19} \\ \end{array} } \right. \)
2 Thruster’s level \( T = 15.0 \)
3 The LPC coefficients in the inner loop \( \left\{ {\begin{array}{*{20}c} {k_{px} = 15.0} \\ {k_{py} = 15.0} \\ {k_{pz} = 15.0} \\ \end{array} } \right. \)
4 The QPDLQR coefficients in the outer loop \( \left\{ {\begin{array}{*{20}c} {k_{px} = 72.0} \\ {k_{py} = 72.0} \\ {k_{pz} = 72.0} \\ \end{array} } \right. \) \( \left\{ {\begin{array}{*{20}c} {k_{dx} = 200.0} \\ {k_{dy} = 200.0} \\ {k_{dz} = 200.0} \\ \end{array} } \right. \)
5 Thruster’s configurations \( \left\{ {\begin{array}{*{20}c} {L = 0.22} \\ {R = 0.45} \\ \end{array} } \right. \)
6 Relay hysteresis \( \varepsilon = 0.1 \)