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插头锥套式空中加油对接过程中受油机的飞行控制律 被引量:4

Flight Control of Receiver Aircraft for Probe-Drouge Aerial Refueling Docking
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摘要 采用基于参考观测器的轨迹跟踪控制方法,实现空中加油过程中受油插头与加油锥套的精确对接.根据受油机插头与加油锥套之间的相对位置,由参考轨迹生成模块实时生成受油机的机动轨迹.通过参考观测器实时估算出受油机期望跟踪的状态量与控制量,再采用全状态反馈控制,使受油机的受油插头与加油锥套对接.仿真结果表明系统具有良好的跟踪控制性能. A reference observer-based tracking controller is designed to achieve successful docking between the drogue of a tanker aircraft and the probe of a receiver aircraft.A reference trajectory generation module is used to turn the relative position between the drogue and the probe into a smooth reference trajectory. An output tracking observer is designed to estimate the feed-forward control signal and the reference states to be tracked,and a full state feedback controller provides accurate tracking.Simulation results show that integration of observer and controller is effective for achieving accurate aerial refueling docking.
作者 袁锁中 刘曌
出处 《应用科学学报》 CAS CSCD 北大核心 2010年第4期436-440,共5页 Journal of Applied Sciences
基金 国家自然科学基金(No.60674100) 南京航空航天大学基本科研业务费专项科研项目基金(No.V1083-031)资助
关键词 空中加油 插头锥套式 参考观测器 飞行控制 aerial refueling probe and drogue reference observer flight control
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参考文献10

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