Design of Variable Structure Control Law of a Guidance Missile

摘要

In this paper, a novel guidance lav based on Line of Sight from the launching station to the target by using variable structure control (VSC) is proposed. The basic feature of VSC is the sliding motion. Sliding Mode Controller (SMC) are robust, simple guidance and control algorithms which can be applied to anti-tank missiles. Here we design the guidance control law for high speed kinetic energy anti-lank missiles (HKEM).