Sliding mode based attitude and acceleration controller for a velocity-varying skid-to-turn missile

Abstract

Sliding mode based roll-pitch-yaw integrated attitude and acceleration controller for a fin-controlled skid-to-turn(STT) missile is proposed. In terms of aerodynamics, the missile model has severe nonlinearities and coupling effect between input channels and roll-pitch-yaw angles that make the controller design challenging. Moreover, the controller should… (More)

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