Cooperative Strategies with Boundary Conditions for Optimal Aircraft Simultaneous Attack

In this study, a distributed guidance law for simultaneous attack of multiple missiles on single target is proposed. The guidance law consists of two components, one component utilizes the optimal control theory and boundary conditions to ensure missile-target relative states converge to zero, while another component keeps the relative states consistent before the simultaneous attack is accomplished. The control inputs and adaptive parameters are optimized by a protocol function to avoid excessively large input. The boundary conditions are designed to ensure the relative states converge to the designer specified values. The simulation results demonstrated the practicability of the proposed guidance law.