Yaw control of maneuvering tailless aircraft using induced drag - a control allocation method based on aerodynamic mode shapes

Yaw control of maneuvering tailless aircraft using induced drag - a control allocation method based on aerodynamic mode shapes
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诱导阻力机动无尾飞机偏航控制——一种基于气动模态振型的控制分配方法

DOI:
10.2514/6.2020-2677
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发表时间:
2020
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通讯作者:
Shearwood T
Shearwood T
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作者:
Shearwood T

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