插头锥管式受油机纵向飞行控制研究  

Longitudinal Flight Control Research for the Receiver with a Probe-Drogue Refueling System

作　　者：陈博[1] 董新民[1] 徐跃鉴[1] 林秦颖[1] 

机构地区：[1]空军工程大学工程学院,陕西西安710038

出　　处：《飞行力学》2008年第1期31-34,共4页Flight Dynamics

摘　　要：分析了空中加油对接过程中受油机受到的各种扰动,阐述了插头锥管加油方式受油机的纵向飞行控制原理。在此基础上,采用μ方法设计了受油机的纵向鲁棒飞行控制律。受油机俯仰角指令的响应结果表明,系统具有较好的跟踪能力和干扰抑制能力。The disturbances acting on the receiver aircraft in the docking phase of an aerial refueling are analyzed and the truth of longitudinal flight control of the receiver is introduced. Then, the longitudinal robust controller is designed with μ method. Finally, the command-tracking simulation of the receiver＇ s pitch angle is made, and the results show that the receiver system has a satisfactory performance of command-tracking and jamming resist-ance.

关 键 词：飞行控制 鲁棒控制 Μ综合 空中加油 插头锥管 

分 类 号：V249.1[航空宇航科学与技术—飞行器设计]