In this paper. considering a class of skid-to-turn (STT) missile with impact angle constraint to intercept the maneuvering target. a three-dimensional integrated guidance and control law based on the fractional integral terminal sliding mode control (FITSMC) scheme is proposed. Firstly. https://www.spidertattooz.com/Veuve-Ambal-Rose-Cremant-de-Bourgogne-750ml/