基于滑模的自主空中加油制导与控制一体化  

Integration of Guidance and Control for Autonomous Aerial Refueling Based on Sliding Mode

作　　者：朱子睿 袁锁中[1] Zhu Zirui;Yuan Suozhong(College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,China)

机构地区：[1]南京航空航天大学自动化学院,南京211106

出　　处：《兵工自动化》2025年第4期47-52,共6页Ordnance Industry Automation

摘　　要：为提高受油机跟踪会合的快速性和准确性,提出一种基于滑模的空中加油制导与控制一体化(integrated guidance and control,IGC)设计方法。为将制导与控制回路关联,采用滑模面整合多个中间控制变量,从而将制导指令转化为所需的舵面输入。通过与传统制导与控制独立设计方法比较,制导控制一体化设计可以有效提升受油机的跟踪性能,缩短会合对接所需的时间。研究结果表明,该设计方法对空中加油系统开发有一定的参考价值。To improve the rapidity and accuracy of receiver aircraft tracking rendezvous,an design method of integrated guidance and control(IGC)for aerial refueling based on sliding mode is proposed.To link the guidance and control loop,a sliding mode surface is used to integrate multiple intermediate control variables to convert the guidance command into the required control surface input.Compared with the traditional independent design method of guidance and control,the integrated design of guidance and control can effectively improve the tracking performance of the receiver aircraft and shorten the time required for rendezvous and docking.The results show that the design method has a certain reference value for the development of aerial refueling system.

关 键 词：空中加油 制导控制一体化 滑模制导 

分 类 号：V249.122[航空宇航科学与技术—飞行器设计]