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Reaction jet thruster provides extra moment in order to change the trajectory of the missile rapidly. However, it will induce interactions between the airflow and the thruster's jet. In this paper, a simple H2 decoupling analytical design under internal model control structure is adapted to a novel designed model of divert controlled missile. Using this model, controller can handle the system uncertainty...
A novel approach combining the sliding mode control and extended state observer is proposed for attitude control of a quaternion missile model which is nonlinear in aerodynamics. Combining the back-stepping technique, the corresponding sliding mode controller is designed to guarantee the state variables of the closed loop system to converge to the reference state with the help of the extended state...
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