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.
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