首页 | 官方网站   微博 | 高级检索  
     

高超声速飞行器命中精度高准确度评估
引用本文:彭维仕.高超声速飞行器命中精度高准确度评估[J].北京航空航天大学学报,2022,48(11):2130-2137.
作者姓名:彭维仕
作者单位:武警工程大学 装备管理与保障学院, 西安 710086
基金项目:国家自然科学基金71801222陕西省自然科学基金2018JQ6019博士后创新人才支持计划BX201700104
摘    要:为科学合理地评估高超声速飞行器的命中精度, 提出了一种基于误差谱的高超声速飞行器命中精度高准确度评估方法。对获得的高超声速飞行器命中精度数据进行预处理, 得到该数据的落点偏差。构建算术平均误差、均方根误差、调和平均误差、误差中位数、误差众数、几何平均误差和迭代中距误差评估指标来反映高超声速飞行器命中精度的性能。分别建立高超声速飞行器命中精度评估模型及其可信度模型。通过实例验证所提评估方法的正确性和合理性。仿真结果表明:所提方法不仅能给出高超声速飞行器命中精度的评估结果, 还能给出该结果的可信度。研究工作为高超声速飞行器命中精度的高准确度评估提供了新的科学评估方法。 

关 键 词:高超声速飞行器    误差谱    系统评论理论与方法    命中精度评估方法    可信度模型
收稿时间:2021-03-01

Evaluation of high hitting accuracy performance of hypersonic vehicle
Affiliation:School of Equipment Management and Support, People Armed Police Engineering University, Xi'an 710086, China
Abstract:To evaluate the hitting accuracy of hypersonic vehicles scientifically and reasonably, this paper proposes a high accuracy evaluation method using the error spectrum. First, the hit accuracy data of hypersonic vehicles are preprocessed to obtain the relative distance error. Secondly, the root mean square, average Euclidean error, harmonic average error, median error, error mode metric, geometric average error and iterative mid-range error are constructed to reflect the hitting accuracy of hypersonic vehicles. Then, we build the high accuracy evaluation model and its credibility model for hypersonic vehicles. Finally, two examples are given to verify the correctness and rationality of the proposed method. The simulation results show that this method can obtain not only the result of the hit accuracy evaluation, but also the credibility of the result. This research provides a new scientific evaluation method for evaluating high hitting accuracy of hypersonic vehicles. 
Keywords:
点击此处可从《北京航空航天大学学报》浏览原始摘要信息
点击此处可从《北京航空航天大学学报》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司    京ICP备09084417号-23

京公网安备 11010802026262号