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

MissileStt MissilesEngineeringAerospace EngineeringGuidance SystemAdaptive ControlSystems EngineeringAerodynamicsStochastic ControlFull StateTrajectory OptimizationNon-affine Aerodynamic Characteristics