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- W1553618521 abstract "In this paper the attitude tracking problem is solved for a flexible spacecraft in the case of measurements of the variables describing the attitude error. Such a control could be applied in failure situations for recovering a spacecraft, so increasing the fault tolerance of the spacecraft control system and the success of the mission. The result is a dynamic controller capable of reconstructing the information regarding the spacecraft angular velocity and those regarding the modal variables, describing the dynamics of the flexible appendages present in the spacecraft." @default.
- W1553618521 created "2016-06-24" @default.
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- W1553618521 date "2003-09-01" @default.
- W1553618521 modified "2023-09-27" @default.
- W1553618521 title "Tracking control using attitude measurements for flexible spacecraft" @default.
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- W1553618521 doi "https://doi.org/10.23919/ecc.2003.7086441" @default.
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