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Saturday, May 16, 2020 | History

3 edition of Theory and computation of optimal low- and medium-thrust transfers found in the catalog.

Theory and computation of optimal low- and medium-thrust transfers

Theory and computation of optimal low- and medium-thrust transfers

semi-annual status report, January 7, 1994 to July 6, 1994

  • 332 Want to read
  • 28 Currently reading

Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC, Springfield, Va .
Written in English

    Subjects:
  • Orbital transfer (Space flight),
  • Rocket engines -- Thrust.

  • Edition Notes

    Statementprincipal investigator/project director, Dr. C-H. Chuang.
    SeriesNASA contractor report -- NASA CR-196077.
    ContributionsUnited States. National Aeronautics and Space Administration.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17682359M

    Full text of "NASA Technical Reports Server (NTRS) NASA university program management information system, FY " See other formats. Full text of "The Second Conference on Lunar Bases and Space Activities of the 21st Century, volume 1" See other formats.

    ,中国空间科学技术 年 10 月 61 第 5 期 Chinese Space Science and T echnology 基于人工免疫算法的 地球一火星小推力转移轨道优化 彭冲l 徐世杰2 采琳丽l 王平1 (1中国空间技术研究院载人航天总体部,北京 ) (2 北京航空航天大学宇航学院,北京


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Another difficult problem, quite new in low-thrust optimal control literature, is the computation of optimal rendezvous—with specific final angular position—between distant orbits. Most of the time, orbits are assumed to be close [13] and even almost circular in order to use the linear theory [14].Cited by: Request PDF | Facets of combinatorial optimization.

Festschrift for Martin Grötschel on the occasion of his 65th birthday | Martin Grötschel is one. Chuang, C.-H.: Theory and computation of optimal low- and medium-thrust orbit transfers.

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Considering the drag of all components, the net increase in propulsive efficiency by the addition of SRV is found to be % for the cruise and % for the medium-thrust condition with a net. Scribd adalah situs bacaan dan penerbitan sosial terbesar di dunia.

This work describes and applies the recently introduced, general-purpose perturbative guidance termed variable-time-domain neighboring optimal guidance, which is capable of driving an aerospace vehicle along a specified nominal, optimal path.

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