Optimal trajectory design for safety rendezvous based on sparse modeling

Satoshi Nagashima; Mai Bando; Shinji Hokamoto

Optimal trajectory design for safety rendezvous based on sparse modeling

Satoshi Nagashima, Mai Bando, Shinji Hokamoto

Research output: Contribution to journal › Conference article › peer-review

Abstract

In trajectory design of a spacecraft, reducing the fuel consumption is important factor. In order to find the minimum fuel trajectory, this paper considers the L¹ norm as the performance index. This paper discuss design parameters characterizing the L¹ optimal trajectory, such as sampling time, flight time and magnitude of thrust. Also, this paper compare with the conventional method from the viewpoint of fuel consumption. In addition, this paper consider the rendezvous problem considering safety.

Original language	English
Journal	Proceedings of the International Astronautical Congress, IAC
Volume	2018-October
Publication status	Published - 2018
Event	69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 - Bremen, Germany Duration: Oct 1 2018 → Oct 5 2018

All Science Journal Classification (ASJC) codes

Aerospace Engineering
Astronomy and Astrophysics
Space and Planetary Science

Cite this

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title = "Optimal trajectory design for safety rendezvous based on sparse modeling",

abstract = "In trajectory design of a spacecraft, reducing the fuel consumption is important factor. In order to find the minimum fuel trajectory, this paper considers the L1 norm as the performance index. This paper discuss design parameters characterizing the L1 optimal trajectory, such as sampling time, flight time and magnitude of thrust. Also, this paper compare with the conventional method from the viewpoint of fuel consumption. In addition, this paper consider the rendezvous problem considering safety.",

author = "Satoshi Nagashima and Mai Bando and Shinji Hokamoto",

note = "Publisher Copyright: Copyright {\textcopyright} 2018 by the International Astronautical Federation (IAF). All rights reserved.; 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 ; Conference date: 01-10-2018 Through 05-10-2018",

year = "2018",

language = "English",

volume = "2018-October",

journal = "Proceedings of the International Astronautical Congress, IAC",

issn = "0074-1795",

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T1 - Optimal trajectory design for safety rendezvous based on sparse modeling

AU - Nagashima, Satoshi

AU - Bando, Mai

AU - Hokamoto, Shinji

PY - 2018

Y1 - 2018

N2 - In trajectory design of a spacecraft, reducing the fuel consumption is important factor. In order to find the minimum fuel trajectory, this paper considers the L1 norm as the performance index. This paper discuss design parameters characterizing the L1 optimal trajectory, such as sampling time, flight time and magnitude of thrust. Also, this paper compare with the conventional method from the viewpoint of fuel consumption. In addition, this paper consider the rendezvous problem considering safety.

AB - In trajectory design of a spacecraft, reducing the fuel consumption is important factor. In order to find the minimum fuel trajectory, this paper considers the L1 norm as the performance index. This paper discuss design parameters characterizing the L1 optimal trajectory, such as sampling time, flight time and magnitude of thrust. Also, this paper compare with the conventional method from the viewpoint of fuel consumption. In addition, this paper consider the rendezvous problem considering safety.

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M3 - Conference article

AN - SCOPUS:85065295868

VL - 2018-October

JO - Proceedings of the International Astronautical Congress, IAC

JF - Proceedings of the International Astronautical Congress, IAC

SN - 0074-1795

T2 - 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018

Y2 - 1 October 2018 through 5 October 2018

ER -

Optimal trajectory design for safety rendezvous based on sparse modeling

Abstract

All Science Journal Classification (ASJC) codes

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