Terminal guidance law design based on predictive control for aerodynamic missile with side window detection

In this paper, terminal guidance problem for aerodynamic missile with side window detection is considered. Firstly, the description of side window constraint is given. In order to formulate this guidance problem as a control problem with input constraint, side window constraint is transformed into attack angle constraint. Then the terminal guidance law is designed based on predictive control. Simulation results are given to show the effectiveness of the proposed guidance law design approach.