Finite-Time Attitude Tracking Control for Spacecraft Using Terminal Sliding Mode and Chebyshev Neural Network
By Anmin Zou, Krishna Dev Kumar, Zeng-Guang Hou, Xi Liu. IEEE Transactions on Systems Man and Cybernetics Part B (Cybernetics), 2011
415 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Control and Systems Engineering
View Paper: https://www.semanticscholar.org/paper/f36d193bb4ba5eb50ea628139d0e9260aba6a334
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In Aerospace Engineering
In Control and Systems Engineering
Citations in the corpus
- Adaptive attitude tracking control for rigid spacecraft with finite-time convergence (2013, positive): “Thus, a modified FTSMS s = ẋ+ k1x+ k2β(x)with s̄ = ẋ + k1x + k2x r1 r2 and constraint in Zou, Kumar, Hou, and Liu (2011) is researched.”
- Robust adaptive finite‐time parameter estimation and control for robotic systems (2015, methodology): “Several researchers [25, 26, 32] have raised this issue; they suggested the use of some smoothening technique.”
- Terminal Sliding Mode Control – An Overview (2021, background): “In [117], a finite-time attitude tracking control scheme was pro-”
- Satellite Attitude Stabilization Control with Actuator Faults (2017, methodology): “Transformed Attitude Dynamics and Sliding-Mode Manifold To address the attitude stabilization problem, the satellite attitude dynamics is rewritten by using a Lagrange-like equation [6,18,19].”