火力与指挥控制2024，Vol.49Issue(2)：56-62,7.DOI:10.3969/j.issn.1002-0640.2024.02.008
无人机天钩回收航迹控制系统设计与实现
The Design and Implementation of Track Control System for UAV Skyhook Recovery
摘要
Abstract
Skyhook recovery of unmanned aerial vehicle(UAV)has higher requirements for control accuracy including track deviation and others.The challenges are proposed for the control system.A new track control method for skyhook recovery of unmanned aerial vehicle(UAV)is proposed.Skyhook recovery control strategy and process of UAV are designed and the composition of control system is proposed.Based on UAV wind tunnel test data,linear and nonlinear model for skyhook recovery of UAV are constructed.The track control law is designed with optimized L1 track control method.The design is applied in real flight test,the correctness and engineering realization of the designed control system are verified.The final flight test results show that the aircraft can be accurately recovered by the designed control system,and has excellent dynamic characteristics.关键词
无人机/天钩回收/风洞试验数据/L1航迹控制Key words
unmanned aerial vehicle/skyhook recovery/wind tunnel test data/L1 track control分类
信息技术与安全科学引用本文复制引用
张剑锋,王朋飞..无人机天钩回收航迹控制系统设计与实现[J].火力与指挥控制,2024,49(2):56-62,7.基金项目
陕西省重点产业创新项目(2009ZDLGY14-06) （2009ZDLGY14-06）
