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固定翼UAV路径跟踪的全局稳定积分滑模S面控制OA北大核心CSTPCD

Path Tracking Controller of Fixed-Wing UAVs Based on Globally Stable Integral Sliding Mode S-Plane Model

中文摘要英文摘要

针对固定翼无人机的三维路径跟踪控制问题,设计了一种基于全局稳定积分滑模S面模型的内外环控制器.控制器外环采用全局稳定积分滑模控制,内环采用S面控制.设计控制器外环的全局稳定积分滑模控制律,并采用Lyapunov理论证明所设计控制律的稳定性.对内环的指令信号设计S面控制器,考虑到S面控制器中求导的复杂性,引入二阶微分器,解决内环中导数存在积分爆炸的问题.半物理仿真试验结果表明,提出的控制器能精确跟踪期望路径,具有良好的控制性能和抗干扰性能.

For the three-dimensional path tracking control problem of fixed-wing unmanned aerial vehicles,an inner and outer loop controller based on globally stable integral sliding mode S-plane model is proposed in this paper.The outer loop is controlled by the globally stable integral sliding mode,and the inner loop is controlled by the S-plane.Firstly,the globally stable integral sliding control law is designed for the outer loop,and the stability of the control law is proved using the Lyapunov theory.Then the S-plane controller is designed for the instruction signal of the inner loop.Due to the complexity of derivation in the S-plane controller,a second-order differentiator is introduced.The simulation results show that the proposed controller can track the ideal path accurately,which has good control performance and anti-interference performance.

陈鹏云;张国兵;李佳成;关通;石上瑶

中北大学 航空宇航学院,太原 030051中北大学 软件学院,太原 030051

计算机与自动化

无人机全局稳定路径跟踪运动控制滑模控制S面控制

unmanned aerial vehicleglobal stabilitypath trackingmotion controlsliding mode controlS-plane control

《计算机工程与应用》 2024 (013)

353-360 / 8

国家自然科学基金(51909245,62003314);山西省重点研发计划(202202020101001);山西省基础研究计划(202103021224187,20210302124010,20210302123050).

10.3778/j.issn.1002-8331.2304-0265

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