Trajectory design of destiny mission

Mai Bando, Masaki Nakamiya, Yasuhiro Kawakatsu, Chikako Hirose, Takayuki Yamamoto

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The trajectory design of the interplanetary mission "Demonstration and Experiment of Space Technology for INterplanetary voYage, DESTINY" is discussed. The trajectory optimization of low-thrust spacecraft pose a difficult design challenge. Moreover, DESTINY mission requires many constraints for the orbital design. In advance of optimizing the whole transfer mission, we investigated the basic theory to design which can take into account such constraints.

Original languageEnglish
Title of host publicationSpace for Our Future - Advances in the Astronautical Sciences
Subtitle of host publicationProceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012
Pages321-322
Number of pages2
Publication statusPublished - 2013
Externally publishedYes
Event13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012 - Kyoto, Japan
Duration: May 15 2012May 18 2012

Publication series

NameAdvances in the Astronautical Sciences
Volume146
ISSN (Print)0065-3438

Other

Other13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012
Country/TerritoryJapan
CityKyoto
Period5/15/125/18/12

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

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