Advanced Search
Volume 33 Issue 04
Apr.  2007
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2007  >  33(04): 388-391.
Shi Jun, Han Chao. Quick algorithm for designing emergency orbital transfer scheme[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(04): 388-391. (in Chinese)
Citation: Shi Jun, Han Chao. Quick algorithm for designing emergency orbital transfer scheme[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(04): 388-391. (in Chinese)
shu

Quick algorithm for designing emergency orbital transfer scheme

  • School of Astronautics, Beijing University of Aeronautics and As tronautics, Beijing 100083, China

  • Received Date: 28 Apr 2006
  • Publish Date: 30 Apr 2007
    Abstract
  • A quick algorithm for designing emergency orbital transfer scheme that can meet the requirements of measure, fuel and time during emergency orbita l transfer was presented. The orbital transfer mode suitable for variable search was given. The question of designing orbital transfer scheme quickly was transf ormed into the question of restricted optimization. And the entire mathematics m odel of measure restrictions was established and the corresponding algorithm for measure restrictions was presented. Orbital transfer scheme, that is required n ot only to meet measure restrictions, but also to achieve optimal goal, was foun d by using genetic algorithm. Cases of calculation show that the orbital transfe r schemes designed by using this quick algorithm can meet the need of emergency orbital transfer mission.

     

    • FullText(HTML)
  • loading
    • References(1)
  • [1] Battin R H, Vaughan R H. An elegant Lambert algorithm . Journal of Guidance and Control, 1984, 7(6):662-670 [2] Battin R H. An introduction to the mathematics and methods of astrodynamics[M]. New York:AIAA Education Series, 1987 [3] Prussing J E. A class of optimal two-impulse rendezvous using multiple-re volution Lambert solutions[J]. Journal of the Astronautical Sciences, 2000, 48 (2):131-148 [4] Shen H, Tsiotras P. Optimal two-impulse rendezvous using multiple-revolution Lambert solutions[J]. Journal of Guidance, Control and Dynamics, 2003, 26 (1):50-61 [5] 韩潮,谢华伟.空间交会中多圈Lambert变轨算法研究[J]. 中国空间科学技术,2004, 24(5):9-14 Han Chao, Xie Huawei. Research on algorithm of loopy Lambert transfer in space rendezvous[J]. Chinese Space Science and Technology, 2004, 24(5):9-14(in Chinese)
    • Relative Articles
    • 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(2516) PDF downloads(999) 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