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• W4387192510 abstract "This paper proposes an adaptive, chatter-free, non-singular fast terminal sliding mode (CNFTSM) control method to solve the fixed-time attitude tracking problem of rigid spacecraft with inertial uncertainty and external disturbances. To ensure the system state converges to the origin within a fixed time, a new fixed-time sliding surface is designed to solve the fixed-time attitude tracking problem, and an adaptive law is introduced to ensure the robustness of trajectory tracking. Finally, simulation results verify the effectiveness of the proposed control strategy." @default.
• W4387192510 created "2023-09-30" @default.
• W4387192510 creator A5060365184 @default.
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• W4387192510 date "2023-08-01" @default.
• W4387192510 modified "2023-09-30" @default.
• W4387192510 title "Adaptive Chatter-Free Non-Singular Fast Terminal Sliding Mode Attitude Control for Rigid Spacecraft" @default.
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• W4387192510 doi "https://doi.org/10.1109/ihmsc58761.2023.00031" @default.
• W4387192510 hasPublicationYear "2023" @default.
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