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• W2790816972 abstract "The robust attitude and vibration control of a flexible spacecraft trying to perform accurate maneuvers in spite of various sources of uncertainty is addressed here. Difficulties for achieving precise and stable pointing arise from noisy onboard sensors, parameters indeterminacy, outer disturbances as well as un-modeled or hidden dynamics interactions. Based on high-order sliding-mode methods, the non-minimum phase nature of the problem is dealt with through output redefinition. An adaptive super-twisting algorithm (ASTA) is incorporated with its observer counterpart on the system under consideration to get reliable attitude and vibration control in the presence of sensor noise and momentum coupling. The closed-loop efficiency is verified through simulations under various indeterminate situations and got compared to other methods." @default.
• W2790816972 created "2018-03-29" @default.
• W2790816972 creator A5013860741 @default.
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• W2790816972 date "2018-05-01" @default.
• W2790816972 modified "2023-10-18" @default.
• W2790816972 title "Adaptive super twisting vibration control of a flexible spacecraft with state rate estimation" @default.
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• W2790816972 doi "https://doi.org/10.1016/j.jsv.2018.02.037" @default.
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