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四旋翼无人机自适应角度刚性编队控制

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针对具有风扰的四旋翼无人机系统,提出一种仅基于角度测量信息的编队控制策略.构建势能函数设计纯方位编队控制策略,并引入参数自适应估计对无人机系统进行补偿,以消除外界风扰对四旋翼无人机系统飞行性能的影响.利用Barbalat's引理验证四旋翼无人机系统可以达到期望的编队形状,并证明多无人机编队系统的全局稳定性.仿真结果表明无人机自适应角度刚性编队控制策略是有效的.
Adaptive bearing rigid formation control for quadrotor UAV
For a quadrotor UAV(unmanned aerial vehicle)system with wind disturbance,a bear-ing-only formation control strategy is proposed.Firstly,the potential energy function is construc-ted to design the bearing rigid formation control strategy.Furthermore,the parameter adaptive estimation is introduced to compensate the system,which eliminates the influence of external wind disturbance on the flight performance of the quadrotor UAV system.Subsequently,Barbalat's Lemma is utilized to verify that the quadrotor UAV system can achieve the desired formation shape,and to prove global stability of the multi-UAV formation system.Ultimately,the simulation out-comes corroborate the efficacy of the adaptive bearing rigid formation control strategy for UAVs.

bearing rigid formation controlmultiple unmanned aerial systemwind disturbanceadaptive estimation algorithm

王芹、耿皓若、殷瀚宇、沈宇航、裔扬

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扬州大学信息工程学院,江苏扬州 225127

角度刚性编队控制 多无人机系统 风扰 自适应估计

2024

扬州大学学报(自然科学版)
扬州大学

扬州大学学报(自然科学版)

影响因子:0.473
ISSN:1007-824X
年,卷(期):2024.27(6)