caa a22 4500 445360313 CHVBK 20180317142913.0 cr unu---uuuuu 170323e20110601xx s 000 0 eng 10.1007/s11071-011-0007-5 doi (NATIONALLICENCE)springer-10.1007/s11071-011-0007-5 Cushman Adam Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, 20723, Laurel, MD, USA aut Rebuttal to "Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness” [Elektronische Daten] [Adam Cushman] A paper, "Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness,” was published in the journal Nonlinear Dynamics. The Lyapunov proof is flawed and does not prove stability for the system. It is also unclear how the simulation results in the paper were obtained using the control law. This rebuttal will demonstrate the flaws in the original paper. Springer Science+Business Media B.V., 2011 Fault tolerant nationallicence Sliding mode control nationallicence Loss of actuator effectiveness nationallicence Nonlinear Dynamics Springer Netherlands 64/4(2011-06-01), 409-411 0924-090X 64:4<409 2011 64 11071 https://doi.org/10.1007/s11071-011-0007-5 text/html Onlinezugriff via DOI 1 brief-communication jats NATIONALLICENCE 856 40 https://doi.org/10.1007/s11071-011-0007-5 text/html Onlinezugriff via DOI NATIONALLICENCE 100 1- Cushman Adam Johns Hopkins University Applied Physics Laboratory, 11100 Johns Hopkins Road, 20723, Laurel, MD, USA aut NATIONALLICENCE 773 0- Nonlinear Dynamics Springer Netherlands 64/4(2011-06-01), 409-411 0924-090X 64:4<409 2011 64 11071 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer