Full State Constrained Stochastic Adaptive Integrated Guidance and Control for STT Missiles with Non-Affine Aerodynamic Characteristics

•A novel stochastic adaptive IGC structure, which can guarantee all of the system states to be constrained and maintain desired guidance performance in the presence of the stochastic disturbances and aerodynamic uncertainties, is developed.•Different from the existing results, in this work the target is permitted to keep rapidly maneuvering with inaccessible and changing target accelerations.•As far as the authors know, it also the first IGC scheme for the STT missiles with the non-affine aerodynamic characteristics taken into consideration.