兵工自动化2025，Vol.44Issue(4)：47-52,6.DOI:10.7690/bgzdh.2025.04.010
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
朱子睿 1袁锁中1
作者信息
- 1. 南京航空航天大学自动化学院,南京 211106
- 折叠
摘要
Abstract
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Key words
aerial refueling/integration of guidance and control/sliding mode guidance引用本文复制引用
朱子睿,袁锁中..基于滑模的自主空中加油制导与控制一体化[J].兵工自动化,2025,44(4):47-52,6.
