航空学报2026，Vol.47Issue(11)：287-303,17.DOI:10.7527/S1000-6893.2026.32793
加油装置空中对接先进控制器设计与风洞试验
Design and wind tunnel test of an advanced controller for aerial refueling docking
摘要
Abstract
A sensitive and robust controller is one of the core technologies for efficient and safe aerial docking.This study focuses on the rapid and precise docking control of a refueling system under complex airflow disturbances.A high-fidelity model of the system with gimbal composite hinge pairs is established.Building upon a controller composed of backstepping control and a sliding mode observer,the design incorporates considerations for embedded hardware transplantation factors,such as onboard models and filter design,thus realizing the design of an advanced aerial docking controller that is hardware-implementable.Finally,through ground simulation tests and wind tunnel flight tests,the dynamic response characteristics of the controller with onboard model dynamic feedback under the two types of test environments were comparatively analyzed.The results provide effective design references for the verifi-cation and development of similar advanced controllers.Furthermore,a comparative analysis of the response differ-ences in docking characteristics between a Proportional-Integral(PI)controller and the advanced disturbance-rejection controller under wind tunnel test conditions was conducted.This analysis indicates the significant advantages of the advanced disturbance-rejection controller in accomplishing the aerial docking mission of the refueling system.关键词
加油/自动对接/抗干扰控制/滑模观测/风洞试验Key words
refueling/auto docking/disturbance-rejection control/sliding mode observer/wind tunnel test分类
航空航天引用本文复制引用
罗飞,蒋彪,高怡宁,胡志勇,刘海良,张军红,苏子康..加油装置空中对接先进控制器设计与风洞试验[J].航空学报,2026,47(11):287-303,17.基金项目
国家自然科学基金(62573232,61903190) National Natural Science Foundation of China(62573232,61903190) （62573232,61903190）
