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• W4286306502 abstract "This paper investigates the problem of attitude tracking control for rigid spacecraft with high precision requirement. Utilizing the fixed-time control theorem, a new fixed-time extended state observer (FTESO) is designed to solve the impacts from overall parameter uncertainties and external disturbances. Using the proposed FTESO, a finite-time controller is then developed based on barrier Lyapunov function (BLF). The control scheme is continuous and nonsingular, and it can guarantee that the attitude tracking error converges to a small origin within finite-time while satisfying attitude constraint. Finally, simulation results are employed to demonstrate the effectiveness of the developed control algorithm." @default.
• W4286306502 created "2022-07-21" @default.
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• W4286306502 date "2022-05-04" @default.
• W4286306502 modified "2023-09-29" @default.
• W4286306502 title "Design of Fixed-Time Extended State Observer for Spacecraft Attitude Tracking" @default.
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• W4286306502 doi "https://doi.org/10.23919/ascc56756.2022.9828098" @default.
• W4286306502 hasPublicationYear "2022" @default.
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