Abstract The attitude stabilization problem for rigid spacecraft in the presence of inertial uncertainties, external disturbances, actuator saturations, and actuator faults is addressed in this chapter. First, a novel fast terminal sliding mode manifold is designed to avoid the singularity problem while providing high control ability. In addition, fast terminal sliding mode control laws are proposed to make the spacecraft system trajectory fast converge onto the fast terminal sliding mode surface, and finally evolve into a small region in finite time, which cannot be achieved by the previous literatures. Based on the real sliding mode context, a practical adaptive fast terminal sliding mode control law is presented to guarantee attitude stabilization in finite time. Also, simulation results are presented to illustrate the effectiveness of the control strategies.
Adaptive Finite-Time Attitude Stabilization for Rigid Spacecraft with Actuator Faults and Saturation Constraints
2018-07-03
22 pages
Article/Chapter (Book)
Electronic Resource
English
Finite-Time Attitude Stabilization for Rigid Spacecraft
Springer Verlag | 2018
|Finite-Time Fault Tolerant Attitude Tracking Control for Rigid Spacecraft with Actuator Saturation
Springer Verlag | 2018
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