This study investigates the hybrid fault-tolerant control (FTC) for hypersonic flight vehicles (HFVs) under the rudder structure fault (RSF) and rudder angle deviation fault (RADF). The nonlinear equations of the model are linearised by fuzzy logic. the external nonlinear disturbance is approximated by radial basis functions. which transforms the classical HFV into a linear system. https://www.benefitlabacademy.com/product-category/north-dakota/