2023
DOI: 10.1007/s11071-023-08695-1
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Prescribed convergence time control of spacecraft attitude dynamics with parametric uncertainty

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Cited by 4 publications
(6 citation statements)
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“…)) are known non-linear functions; w = M −1 (x 1 )F u denotes the disturbances and system uncertainties, which satisfies |w| ≤ b where b is a positive scalar; and u ∈ R is the control input. Through the application of Theorem 1, a standard predefined-time controller design method is presented here based on the sliding mode control technique for system (17). In the control framework, a new predefined-time sliding mode surface is first designed using piecewise function methods, in order to avoid potential singularities.…”
Section: Standard Predefined-time Controller Designmentioning
confidence: 99%
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“…)) are known non-linear functions; w = M −1 (x 1 )F u denotes the disturbances and system uncertainties, which satisfies |w| ≤ b where b is a positive scalar; and u ∈ R is the control input. Through the application of Theorem 1, a standard predefined-time controller design method is presented here based on the sliding mode control technique for system (17). In the control framework, a new predefined-time sliding mode surface is first designed using piecewise function methods, in order to avoid potential singularities.…”
Section: Standard Predefined-time Controller Designmentioning
confidence: 99%
“…Therefore, there is no singularity for the term ΦV q 1 x 1 when an appropriate q is selected. For system (17), the control input u is designed as…”
Section: Standard Predefined-time Controller Designmentioning
confidence: 99%
See 3 more Smart Citations