Large angle attitude control law is investigated in this paper for agile turn of an advanced air-to-air missile that has high off-boresight or over the shoulder capability.
英
美
释义
为研究具有大离轴角及越肩发射能力的先进空空导弹敏捷转弯方法,研究了空空导弹的大角度姿态机动控制律。
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