舰载机着舰纵向非仿射模型控制器设计  被引量:1

Designer of non-affine model controller for carrier-based longitudinal landing

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作  者:张杨[1] 吴文海[1] 胡云安[2] 高丽[1] ZHANG Yang;WU Wenhai;HU Yunan;GAO Li(Department of Aeronautical Instument and Electric Control System, Naval Aeronautical and Astronautical University Qingdao Branch, Qingdao 266041 , China;Department of Control Engineering, Naval Aeronautical and Astronautical University, Yantai 264001 , China)

机构地区:[1]海军航空工程学院青岛校区航空仪电控制系,山东青岛266041 [2]海军航空工程学院控制工程系,山东烟台264001

出  处:《系统工程与电子技术》2018年第3期635-642,共8页Systems Engineering and Electronics

基  金:国家自然科学基金(60674090;51505491)资助课题

摘  要:针对舰载机着舰的纵向非仿射模型,考虑舰尾流扰动的影响,提出基于非仿射模型的预设性能的控制律方法。与传统反演方法通过设置假设条件将舰载机模型转换成仿射形式不同,将舰载机模型转换为更一般的非仿射形式,放宽了假设条件,并在此模型基础上设计控制律方法,使高度、迎角、俯仰角和俯仰角速率等误差满足预先设定的范围。该方法减少了计算量,控制器结构更加简单,同时对舰尾流扰动具有较强的鲁棒性,提高了着舰航迹精度。A new control method based on prescribed performance is proposed for non-affine model during landing,while considering the impact of the airwake disturbance.In contrast to the traditional backstepping method that the carrier model should be transformed into an affine form by setting the hypothesis condition,the proposed method transforms the carrier-based model into a more general non-affine pure feedback form and relaxes the assumptions.The proposed control scheme is capable of guaranteeing tracking errors of height,velocity,altitude,pitch angle,and pitch rate with the prescribed performance.The presented controller possesses much lower computational costs,while has strong robustness for the airwake disturbance,and improves the accuracy of the landing tracking.

关 键 词:舰载机着舰 纵向控制律 非仿射模型 预设性能 

分 类 号:V249.1[航空宇航科学与技术—飞行器设计]

 

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