TY - JOUR
T1 - Optimal trajectory design for safety rendezvous based on sparse modeling
AU - Nagashima, Satoshi
AU - Bando, Mai
AU - Hokamoto, Shinji
N1 - Publisher Copyright:
Copyright © 2018 by the International Astronautical Federation (IAF). All rights reserved.
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
SN - 0074-1795
VL - 2018-October
JO - Proceedings of the International Astronautical Congress, IAC
JF - Proceedings of the International Astronautical Congress, IAC
T2 - 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018
Y2 - 1 October 2018 through 5 October 2018
ER -