Trajectory design of destiny mission

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

Trajectory design of destiny mission

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

Research output: Chapter in Book/Report/Conference proceeding › Conference 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 language	English
Title of host publication	Space for Our Future - Advances in the Astronautical Sciences
Subtitle of host publication	Proceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012
Pages	321-322
Number of pages	2
Volume	146
Publication status	Published - Apr 24 2013
Externally published	Yes
Event	13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012 - Kyoto, Japan Duration: May 15 2012 → May 18 2012

Other

Other	13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012
Country/Territory	Japan
City	Kyoto
Period	5/15/12 → 5/18/12

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Space and Planetary Science

Cite this

Bando, M, Nakamiya, M, Kawakatsu, Y, Hirose, C & Yamamoto, T 2013, Trajectory design of destiny mission. in Space for Our Future - Advances in the Astronautical Sciences: Proceedings of the 13th International Conference of Pacific-Basin Societies, ISCOPS 2012. vol. 146, pp. 321-322, 13th International Space Conference of Pacific-Basin Societies, ISCOPS 2012, Kyoto, Japan, 5/15/12.

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author = "Mai Bando and Masaki Nakamiya and Yasuhiro Kawakatsu and Chikako Hirose and Takayuki Yamamoto",

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AU - Bando, Mai

AU - Nakamiya, Masaki

AU - Kawakatsu, Yasuhiro

AU - Hirose, Chikako

AU - Yamamoto, Takayuki

PY - 2013/4/24

Y1 - 2013/4/24

N2 - 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.

AB - 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.

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Y2 - 15 May 2012 through 18 May 2012

ER -

Trajectory design of destiny mission

Abstract

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All Science Journal Classification (ASJC) codes

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