Based on the characteristics of flying wing UAVs, crosswind landing control systems were designed through the crabbed method and the side-slipping method.

 
  • 摘要針對飛翼無(wú)人機的特性,利用側航法和側滑法設計了側風(fēng)著(zhù)陸控制系統,仿真了系統抗側風(fēng)干擾的能力并進(jìn)行了對比分析。
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