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人工智能气动特性预测技术在火箭子级落区控制项目的应用
引用本文:杜涛,许晨舟,王国辉,宫宇昆,何巍,牟宇,李舟阳,沈丹,程兴,高家一,韩忠华.人工智能气动特性预测技术在火箭子级落区控制项目的应用[J].宇航学报,2021,42(1):61-73.
作者姓名:杜涛  许晨舟  王国辉  宫宇昆  何巍  牟宇  李舟阳  沈丹  程兴  高家一  韩忠华
作者单位:1. 北京宇航系统工程研究所,北京 100076;2. 西北工业大学航空学院翼型、叶栅空气动力学重点实验室,西安 710072
基金项目:国家自然科学基金(11772261)
摘    要:发展了一种基于人工智能算法的气动特性预测技术,在开展部分工况风洞试验基础上,结合少量数值仿真结果,通过机器学习模型预测全部工况气动特性.该方法能够降低研制成本,缩短周期.先后解决了相关函数选择、模型超参数训练、数据检验和"人在回路"应用等关键算法与技术问题,应用于运载火箭子级栅格舵落区控制项目气动研制,获得了设计所需完...

关 键 词:人工智能  机器学习  气动特性  栅格舵  火箭子级落区控制  技术分级
收稿时间:2020-05-13

The Application of Aerodynamic Coefficients Prediction Technique via Artificial Intelligence Method to Rocket First Stage Landing Area Control Project
DU Tao,XU Chen zhou,WANG Guo hui,GONG Yu kun,HE Wei,MOU Yu,LI Zhou yang,SHEN Dan,CHENG Xing,GAO Jia yi,HAN Zhong hua.The Application of Aerodynamic Coefficients Prediction Technique via Artificial Intelligence Method to Rocket First Stage Landing Area Control Project[J].Journal of Astronautics,2021,42(1):61-73.
Authors:DU Tao  XU Chen zhou  WANG Guo hui  GONG Yu kun  HE Wei  MOU Yu  LI Zhou yang  SHEN Dan  CHENG Xing  GAO Jia yi  HAN Zhong hua
Institution:1. Beijing Institute of Astronautical Systems Engineering, Beijing 100076, China; 2. National Key Laboratory of Science and  Technology on Aerodynamic Design and Research, School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China
Abstract:A novel approach of predicting aerodynamic data via artificial intelligence technique is proposed in this article. Based on wind tunnel tests of partial test states, combined with several CFD results, machine learning via Kriging model is used to predict the whole aerodynamic characteristics to shorten the development cycle and reduce the expensive wind tunnel tests as many as possible. After solving several key technical problems such as the selection of correlation functions, hyper parameters training, data verification and application of “man in loop” technique, the complete set of aerodynamic data was obtained successfully and used to the control law design in the rocket first stage landing area control project with grid fins. The correctness of the proposed method was validated by a flight test on 26th July, 2019, which was carried out successfully for the first time in China. At the end, the grading of technology maturity degree for the artificial intelligence technique is presented to evaluate application to aerodynamic engineering design problems.
Keywords:     Artificial intelligence  Machine learning  Aerodynamic  characteristics  Grid fin  Rocket first stage landing area control  Technology  classification       
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