复合翼无人机横侧向控制律设计

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中图分类号：V279 文献标志码：B 文章编号：1671-5276（2025）05-0228-06

Abstract： This study，focusing on the lateral control problem of hybrid UAV，takes a certain typeof hybrid UAV as the researchobjectforcharacteristicanalysis，finding thattheUAVissensitive tocrosswinds.Tworollchannelcontrol strategies were proposed，on which comparison and analysis were made.And therollanglecontrol strategy was selected basedonthe command inner loop，the inner and outer loop parameters were designed by combining the root trajectory and timedomain response，and sideslip angle feedforward strategy was designed to improve the rolltorque suppression effectof the command inner loop on crosswind. Simulation analysis shows that the designed strategy significantly improves its ability to combat crosswinds.

Keywords：hybrid UAV;crosswind sensitivity； lateral control law； sideslip angle feedforward

0 引言

复合翼垂直起降无人机采用旋翼和固定翼相结合的复合设计，能够像直升机一样实现垂直起降和空中悬停，也能够像固定翼飞机一样高速巡航 [1-4] 。（剩余6031字）