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- W2064004705 abstract "In the paper “Quasi-continuous higher order sliding-mode controllers for space-attitude-tracking maneuvers” (IEEE Trans. Ind. Electron., vol. 57, no. 4, pp. 1436–1444, Apr. 2010), higher order sliding-mode control laws are applied to the attitude-tracking maneuvers of spacecraft. It is pointed out in the author's comments that the proposed applications of higher order sliding-mode control, although in the form of second- and third-order sliding-mode controls, can only realize first-order sliding-mode dynamics because of the improperly chosen sliding vectors. The proposed sliding vectors in the paper are suitable when integrators or a first-order lag is added into the system. In the author's comments, alternative measures to realize second- and third-order sliding-mode dynamics are suggested." @default.
- W2064004705 created "2016-06-24" @default.
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- W2064004705 date "2013-07-01" @default.
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- W2064004705 title "Comments on “Quasi-Continuous Higher Order Sliding-Mode Controllers for Spacecraft-Attitude-Tracking Maneuvers”" @default.
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- W2064004705 doi "https://doi.org/10.1109/tie.2012.2196012" @default.
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