Modelling and simulation of an aerial vehicle steering to hit on top of the target at terminal trajectory

In this paper, combined attitude control of the terminal trajectory for an aerial vehicle is presented. The combined attitude controller includes the fuzzy adaptive aerodynamic force mode control and the direct lateral thrust mode control. The dynamic and kinematics mathematical models of the aerial vehicle are built based on the designed reaction-jet control scheme. Simulation results show that the combined control system can satisfy the requirements of the aerial vehicle overload better than the traditional mode does.