Abstract In this chapter, an adaptive fast terminal sliding mode control law (AFTSMCL) is presented to resolve attitude tracking control problem for rigid spacecraft, which can provide finite-time convergence, strong robustness, and fault-tolerant control. A rigorous proof is achieved first. Simulation results are presented to illustrate the effectiveness of presented control law.
Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults
03.07.2018
29 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Finite-Time Fault Tolerant Attitude Tracking Control for Rigid Spacecraft with Actuator Saturation
Springer Verlag | 2018
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