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Adaptive Finite-Time Control for Spacecraft by brian54471 is a document available to read on EtoBox.
What is Adaptive Finite-Time Control for Spacecraft about?
This paper addresses the finite-time attitude tracking control for rigid spacecraft, proposing a novel fast nonsingular terminal sliding mode surface (FNTSMS) that avoids singularity issues while ensuring rapid convergence and high control precision. The control laws developed are continuous and chattering-free, demonstrating robustness against external disturbances and inertia uncertainties. Simulation results validate the effectiveness of the proposed control strategies, including applications to the Hubb
- Author
- brian54471
- Language
- EN