Advanced Search
Volume 41 Issue 11
Nov.  2015
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2015  >  41(11): 2061-2066.
Liu Keyan, Li Yunhua, Sheng Wanxinget al. Optimal research of distributed parallel genetic algorithm for reactive power optimization[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(01): 27-30. (in Chinese)
Citation: SONG Xin, ZHANG Youwei, LIU Zijunet al. Inverse heat conduction problem for transient external heat flux inversion of spacecraft on orbit[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2061-2066. doi: 10.13700/j.bh.1001-5965.2014.0719(in Chinese)
shu

Inverse heat conduction problem for transient external heat flux inversion of spacecraft on orbit

doi: 10.13700/j.bh.1001-5965.2014.0719

  • Beijing Institute of Spacecraft System Engineering, Beijing 100094, China

  • Received Date: 18 Nov 2014
  • Rev Recd Date: 25 Feb 2015
  • Publish Date: 20 Nov 2015
    Abstract
  • Spacecraft external heat flux is very important for researching deterioration law of thermal control coating on orbit, influence of various spatial factors on thermal control products, as well as plume thermal effect of spacecraft attitude and orbit control engine. However, there are many difficulties in direct heat flux measurement. Thus, the inverse heat conduction problem can be used to get results which can satisfy certain precision. Firstly, in order to deduce transient external heat flux of spacecraft on orbit from telemetry temperature of spacecraft equipment on orbit, inverse heat conduction problem mathematical model was set up and solved by the conjugate gradient method. Iterative process of conjugate gradient method was improved according to physics concept in order to increase its anti instabilit. Then, two numerical tests were used for the purpose of checking mathematical model effect. The numerical tests could represent external heat flux change of most both earth-orbiting spacecraft and deep space exploration spacecraft. The maximum relative deviation between inversion value and true value is 2.9% except step change data. Inversion results of the mathematical model is very good. Furthermore, satisfied results can be obtained by processing data analysis for absorbed external heat flux at step change location.

     

    • FullText(HTML)
    • References(16)
  • [1]
    张天宇,董长虹.基于自适应反演法的导弹直/气复合制导[J].北京航空航天大学学报, 2013, 39(7):902-906. Zhang T Y, Dong C H.Compound control system design based on adaptive backstepping theory[J].Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(7):902-906(in Chinese).
    [2]
    杨尔辅,张振鹏,刘国球.一种推进系统故障诊断反问题模型与算法[J].北京航空航天大学学报, 1999, 25(6):684-687. Yang E F, Zhang Z P, Liu G Q.Model and algorithm of inverse-problems on fault diagnosis for propulsion systems[J].Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(6):684-687(in Chinese).
    [3]
    程文龙,刘娜,钟奇,等.卫星稳态热模型参数修正方法研究[J].宇航学报, 2010, 31(1):270-275. Cheng W L, Liu N, Zhong Q, et al.Study on parameters correction method of steady-state thermal model for spacecraft[J].Journal of Astronautics, 2010, 31(1):270-275(in Chinese).
    [4]
    程文龙,刘娜,李志,等.卫星热模型蒙特卡罗混合算法的修正方法应用研究[J].科学通报, 2010, 55(20):2056-2061. Cheng W L, Liu N, Li Z, et al.Application study of a correction method for a spacecraft thermal model with a Monte-Carlo hybrid algorithm[J].Chinese Science Bulletin, 2010, 55(20):2056-2061(in Chinese).
    [5]
    杨沪宁,钟奇.航天器热模型蒙特卡罗法修正论述[J].航天器工程, 2009, 18(3):53-58. Yang H N, Zhong Q.Monte-Carlo method for thermal model correction of spacecraft[J].Spacecraft Engineering, 2009, 18(3):53-58(in Chinese).
    [6]
    张镜洋,常海萍,王立国.小卫星瞬态热分析模型修正方法[J].中国空间科学技术, 2013, 33(4):24-30. Zhang J Y, Chang H P, Wang L G.Correction method for transient thermal analysis model of small satellite[J].Chinese Space Science and Technology, 2013, 33(4):24-30(in Chinese).
    [7]
    张中礼,李明海,胡绍全.外壁热流响应计算的导热反问题方法及其验证[J].强度与环境, 2009, 36(4):54-59. Zhang Z L, Li M H, Hu S Q.Nonlinear transient inverse heat conduction problems method of calculating the boundary heat response[J].Structure & Environment Engineering, 2009, 36(4):54-59(in Chinese).
    [8]
    Lin D T, Yan W M, Li H Y.Inverse problem of unsteady conjugated forced convection in parallel plate channels[J].International Journal of Heat and Mass Transfer, 2008, 51(5-6):993-1002.
    [9]
    Chen U C, Cheng W J, Hsu J C.Two-dimensional inverse problem in estimating heat flux of pin fins[J].International Communication of Heat and Mass Transfer, 2001, 28(6):793-801.
    [10]
    Huang C H, Wang S P.A three-dimensional inverse heat conduction problem in estimated surface heat flux by conjugate gradient method[J].International Journal of Heat and Mass Transfer, 1999, 42(18):3387-3403.
    [11]
    Huang C H, Chen W C.A three-dimensional inverse forced convection problem in estimating surface heat flux by conjugate gradient method[J].International Journal of Heat and Mass Transfer, 2000, 43(17):3171-3181.
    [12]
    薛齐文,杨海天,胡国俊.共轭梯度法求解瞬态传热组合边界条件多宗量反问题[J].应用基础与工程科学学报, 2004, 12(2):113-120. Xue Q W, Yang H T, Hu G J.Solving inverse heat conduction problems with multi-variables of boundary conditions in transient-state via conjugate gradient method[J].Journal of Basic Science and Engineering, 2004, 12(2):113-120(in Chinese).
    [13]
    Xue Q W, Yan H T.A conjugate gradient method for the hyperbolic inverse heat conduction problem with multi-variables[J].Chinese Journal of Computational Physics, 2005, 22(5):417-424.
    [14]
    杨海天,胡国俊.共轭梯度法求解多宗量稳态传热反问题[J].应用基础与工程科学学报, 2002, 10(2):174-181. Yang H T, Hu G J.Solving inverse heat conduction problems with multi-variables in steady-state via conjugate gradient method[J].Journal of Basic Science and Engineering, 2002, 10(2):174-181(in Chinese).
    [15]
    王登刚,刘迎曦,李守巨,等.非线性二维稳态导热反问题的一种数值解法[J].西安交通大学学报, 2000, 34(1):49-52. Wang D G, Liu Y X, Li S J, et a1.Two dimensional numerical solution for nonlinear inverse steady heat conduction[J].Journal of Xi'an Jiaotong University, 2000, 34(1):49-52(in Chinese
    [16]
    范春利,孙丰瑞,杨立.基于红外侧温的试件内部缺陷的识别算法研究[J].工程热物理学报, 2007, 28(2):304-306. Fan C L, Sun F R, Yang L.An algorithm study on identification of subsurface defect based on thermographic temperature measurement[J].Journal of Engineering Thermophysics, 2007, 28(2):304-306(in Chinese).
    • Relative Articles

  • Relative Articles

    [1]LIU He, WEI Cheng, ZHANG Zexu, SUN Bo, HU Zihang. Spacecraft Anomaly Detection Based on Filtered Autoencoder Envelope Analysis[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0832
    [2]GUO Z J，LU H，LIU N，et al. Total ionizing dose effect analysis and radiation hardening design method of Buck-Boost converter[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：389-396 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0050.
    [3]ZHANG Y P，BIAN Q，YANG R Z，et al. Evaluation method of H2O penetration depth of drying reactor based on temperature gradient[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3123-3130 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0764.
    [4]DAI W，SHI S Z，FU Y C，et al. Numerical study on flow and heat transfer of supercritical carbon dioxide under non-uniform heat flux influences[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3074-3083 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0769.
    [5]HUANG Y Z，QUAN Y K，XU G Q，et al. Transient heat flow measurement method based on Laplace transform[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3834-3841 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0904.
    [6]ZHANG Xu, ZHAO Rui, LI Yu, YANG Guang, WANG Li-yan. Component of gas-injection effects on wall heat flux and skin-friction of vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0009
    [7]WANG J D，WANG X，TIAN Y R，et al. Threat assessment of radar radiation sources based on behavioral characteristics[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3196-3207 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0848.
    [8]ZHU C C，TANG Z L，ZHAO X，et al. Multi-objective hybrid algorithm based on gradient search and evolution mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（6）：1940-1951 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0544.
    [9]CAI H，SHI P. Attitude control method for flexible spacecraft based on LPV model[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（12）：3921-3929 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0880.
    [10]JIN L，YANG S L. Fault-tolerant control of spacecraft attitude with prescribed performance based on reinforcement learning[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（8）：2404-2412 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0666.
    [11]LUO Wudi, REN Junxue, LI Zhihui, TANG Haibin. Study on radiation characteristics of multi-phase plumes containing ice crystals in orbit-control engines[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0439
    [12]YAN Pan, LI Qin, HUANG Xiao, GUO Xiao-ming, WENG Yi-hui, YOU Yan-cheng. Research on friction and heat flux prediction of lift-body under different gas models and slip boundary models[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0209
    [13]WU Y，KONG L，SUN Q Q，et al. Heat transfer path design and heat flow analysis of satellite phased array antenna[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1127-1134 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0373.
    [14]SHI Z，WANG B，YANG B，et al. Single-event radiation hardening method for 14 nm pFinFET device[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3335-3342 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0071.
    [15]TAN Chuan-rui, LI Tang, CHEN Wen-qian, WANG Feng, YANG Dong-kai, WU Shi-yu. Evaluation of TDOA Based Air Target Localization Algorithm Using GNSS-Based Passive Radar[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0685
    [16]YANG M，WANG L，YU F，et al. Design and on-orbit application of radiator for space optical remote sensor with large aperture[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（12）：3293-3302 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0116.
    [17]HE J J，YUAN C Q，GONG S P，et al. Sliding mode control for formation flying near libration points using hybrid propulsion[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（5）：1222-1230 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0420.
    [18]LIU Y，ZHOU J P，ZHANG X T. Application and prospect of additive manufacturing technology in manned space engineering[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（1）：83-91 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0455.
    [19]NIE X H，JIN L. Application of kernel principal component analysis in autonomous fault diagnosis for spacecraft flywheel[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（8）：2119-2128 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0582.
    [20]SU Donglin, CUI Shuo, BAI Jiangfei, LI Yaoyao. Fast prediction method for radiated and scattered coupled fields in complex electromagnetic environment[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1553-1560. doi: 10.13700/j.bh.1001-5965.2022.0705
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(967) PDF downloads(393) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return