Open Access

表5

折叠翼飞行器的不确定性参数分布

参数 分布类型 均值 方差
主动力矩系数CA 正态分布 1 0.100
阻力矩系数CR 正态分布 1 0.300
机翼转动惯量I/(kg·m2) 正态分布 7.5 0.015
展开时的攻角α/(°) 正态分布 5.25 1.323

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