Satisfactory results in the design of the BTT missile autopilot are obtained by using this method.

使用这种方法设计BTT导弹自动驾驶仪获得了满意的结果.

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To simplify the robustness design of missile autopilot, an optimization method in time domain is proposed.

为了简化实际中控制系统鲁棒性的设计, 提出一种有约束多目标最优化的鲁棒性时域设计方法.

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