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Table 2 The verification of the proposed control strategy performance w. r. t. the corresponding benchmarks

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

  The approach titles Maximum three-axis rotational angles errors in steady state (deg) Maximum three-axis angular rates errors in steady state (deg/s) Trajectory convergence time (s)
1 The proposed approach Less than 3 Less than 4 Less than 10
2 The Wu approach [15] Less than 5 Less than 6 Less than 25
3 The Butyrin approach [16] Less than 4 Less than 3 Less than 15