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作 者:梁玉峰 赵景朝 刘旺魁 王雷 王世鹏 阮仕龙 LIANG Yufeng;ZHAO Jingchao;LIU Wangkui;WANG Lei;WANG Shipeng;RUAN Shilong(College of Aeronautics and Astronautics,Dalian University of Technology,Dalian 116024,China;Beijing Aerospace Technology Research Institute,Beijing 100074,China;Shenyang Aircraft Design&Research Institute,Shenyang 110035,China)
机构地区:[1]大连理工大学航空航天学院,辽宁大连116024 [2]北京空天技术研究所,北京100074 [3]沈阳飞机设计研究所,辽宁沈阳110035
出 处:《系统工程与电子技术》2023年第9期2866-2872,共7页Systems Engineering and Electronics
基 金:国家自然科学基金(U2141229);航空科学基金(2019ZC063001)资助课题。
摘 要:现代空战环境趋于复杂化,而传统方法对于机动目标难以获得理想的导引效果。因此,针对现代无人机空战导引问题,提出了一种基于顶层滚动优化和底层跟踪的空战导引方法。其中,基于高斯伪谱法的顶层优化以时间为性能指标,快速将无人机导引到目标区域,当目标机动时,对其轨迹进行预测并重新优化导引轨迹。此外,引入对导引视线角的底层跟踪方法,从而完成目标偏航后的快速修正。最后,针对某型作战无人机进行空战环境下的滚动优化导引以及视线角跟踪仿真,验证了所提方法对不确定性机动目标的拦截能力。The modern air combat environment tends to be complicated,and it is difficult for traditional methods to obtain the ideal guidance effects for maneuvering targets.Therefore,an air combat guidance method based on top-level rolling optimization and bottom-level tracking is proposed for the modern unmanned aerial vehicle(UAV)air combat guidance problem.Among them,the top-level optimization based on the Gaussian pseudo-spectral method uses time as the performance index to quickly guide the UAV to the target area.When the target maneuvers,its trajectory is predicted and the guidance trajectory re-optimized.In addition,the underlying tracking method for the guide line of sight angle is introduced,so as to complete the rapid correction after the target yaw.Finally,the simulation of rolling optimal guidance and line of sight angle tracking in the air combat environment is carried out for a certain type of combat UAV,which verifies the interception ability of uncertain maneuvering targets of the proposed method.
分 类 号:V249[航空宇航科学与技术—飞行器设计]
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