A Blended Autopilot for Dual Control Missile Using Generalized P...

A blended autopilot algorithm is developed using generalized predictive control and adaptive<br>non-singular terminal sliding mode control, for dual control missile steered by combination of<br>aerodynamic fins and reaction jets. The blended algorithm considers the reaction jets control design prior<br>due to its inherent control error, and then treats the aerodynamic fin control on the basis of the reaction<br>jets control results. The generalized predictive control method is applied to