Volume 33 Issue 03
Mar.  2007
Turn off MathJax
Article Contents
Chen Tong, Xu Shijie. Optimal Lambert two-impulse transfer using genetic algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(03): 273-277. (in Chinese)
Citation: Chen Tong, Xu Shijie. Optimal Lambert two-impulse transfer using genetic algorithm[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(03): 273-277. (in Chinese)

Optimal Lambert two-impulse transfer using genetic algorithm

  • Received Date: 18 Apr 2006
  • Publish Date: 31 Mar 2007
  • Numerical solutions of Lambert two-impulse orbital transfer with unfi x ed initial position and transfer time were studied. The velocity increment versu s initial position and transfer time were showed in the 3-dimensional plots or 2 -dimensional sections, which are valuable for the practical designing tasks. Base d on the numerical solutions, the optimization problem of Lambert two-impulse or b ital transfer was then proposed and solved by genetic algorithm(GA). The goal w as to find the optimal initial position and transfer time to minimize the weight ed sum of fuel and time. This method was tested in two examples: one was the fue l optimal transfer between coplanar circular orbits, in which the computing resu lt based on GA was compared with that of Hohmann transfer. Another was the fuel and time optimal transfer between elliptical orbits of restricted initial positi on. Results indicate that GA is valid to solve the optimal transfer problems.

     

  • loading
  • [1] Shen Haijun, Tsiotras P. Optimal two-impulse rendezvous using multiple-revolution Lambert solutions[J]. Journal of Guidance, Control, and Dynamics, 2003,26(1):50-61 [2] 韩潮,谢华伟.空间交会中多圈Lambert变轨算法研究[J].空间科学技术,2004,5:9-14 Han Chao, Xie Huawei. Research on algorithm of loopy Lambert transfer in space rendezvous[J]. Chinese Space Science and Technology, 2004,5:9-14(in Chinese) [3] Spencer D B, Kim Y H. Optimal spacecraft rendezvous using genetic algorithms[J]. Journal of Spacecraft and Rockets, 2002, 39(6):859-865 [4] 刘鲁华,汤国建.基于进化算法的空间交会最优轨道机动 全国第十一届空间及运动体控制技术学术会议. 云南:中国宇航学会, 2004:166-170 Liu Luhua, Tang Guojian. Optimal orbital maneuvers of space rendezvous using genetic algorithms Proceedings of the 11th Chinese Biennial Academic Conference on Space/Motion-Bodies Control Technology. Yunnan:Chinese Society of Astronautics, 2004:166-170(in Chinese) [5] 郗晓宁,王威,高玉东.近地航天器轨道基础[M].长沙:国防科技大学出版社,2003:219-235 Xi Xiaoning, Wang Wei, Gao Yudong. Fundamentals of near-earth spacecraft orbit[M]. Changsha:University of National Defence Technology Press, 2003:219-235(in Chinese) [6] 王小平,曹立明.遗传算法——理论、应用与软件实现[M].西安:西安交通大学出版社,2002 Wang Xiaoping, Cao Liming. Genetic algorithms——theory, application and software realization[M]. Xi-an:Xi-an Jiaotong University Press, 2002(in Chinese)
  • 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

    Article Metrics

    Article views(3045) PDF downloads(1283) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return