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Attitude Control of Missile with Time-delay

【摘要】:正In this paper the Fliess expansion is used for attitude control of missile to consider the case when the control is piece-wise. In practice,the control can only be realized with two modifications: (i) instead of rectangle controls "we can only have trapezoid controls"; (ii) the controls must have certain time delay. In this paper the tracking problem via delayed trapezoid controls is considered. The theoretical results are applied to the attitude control of missiles.

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