Synthesis of the Anti-Ship Missile Homing System while Ensuring an Acceptable Oscillation Index of the Stabilization System

Abstract: The paper presents the comparative estimates of the missile homing system using the method of proportional approach and the missile homing system using the direct guidance method with anticipation while firing of low-speed targets, on the basis of which the direct guidance method with anticipation is chosen to build an anti-ship missile homing system. The method of synthesizing the anti-ship missile homing system in the MATLAB environment is described, while ensuring its minimum guidance error and an acceptable oscillation index of the angle stabilization system. © 2022, Allerton Press, Inc.