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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