Review Article

Adaptive Fixed-Time Nonsingular Terminal Sliding Mode Attitude Tracking Control for Spacecraft with Actuator Saturations and Faults

Table 2

The results on comparison of different controllers.

FNTSM control law performance(17) in this paper(25) in [24]

Quaternion error
Angular velocity error
FNTSM/NFTSM error
Convergence time(s)9.9711.01