Rajabi, Mohammad Javad

[ 1 ] - Design of integrated Guidance and control system in the pitch channel using observer based chattering free sliding mode theory

The design of integrated guidance and control system for flying objects is one of the research fields in the aerospace that is considered by researchers in recent years. Due to the nonlinearity of the kinematic and dynamic equations of the homing interceptors in the terminal phase and also existence of uncertainties such as target maneuvers, external disturbances and variations in aerodynamic c...