This paper uses model-following VSCS to construct a parameter-insensitive control system with good disturbance rejection that accepts all command inputs, including those within the nominal input channels. Given an ideal response model, a design method drives plant-model error to obtain a robust sliding mode. This nonlinear control system achieves and maintains sliding mode. Through model -following VSCS, conventional aircraft’s lateral transnational pointing control system is demonstrated.An investigation of the multimode control system's performance in a range of flying conditions, demonstrates the robustness requirements.This topic challenges the proposed technique using ideal response model.

Model-Following VSCS, Aircraft, Sliding Mode Control