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 L 1 norm as the performance index. This paper discuss design parameters characterizing the L 1 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 - Jan 1 2018 |
| Event | 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018 - Bremen, Germany Duration: Oct 1 2018 → Oct 5 2018 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Astronomy and Astrophysics
- Space and Planetary Science
Cite this
Optimal trajectory design for safety rendezvous based on sparse modeling. / Nagashima, Satoshi; Bando, Mai; Hokamoto, Shinji.
In: Proceedings of the International Astronautical Congress, IAC, Vol. 2018-October, 01.01.2018.Research output: Contribution to journal › Conference article
}
TY - JOUR
T1 - Optimal trajectory design for safety rendezvous based on sparse modeling
AU - Nagashima, Satoshi
AU - Bando, Mai
AU - Hokamoto, Shinji
PY - 2018/1/1
Y1 - 2018/1/1
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 L 1 norm as the performance index. This paper discuss design parameters characterizing the L 1 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 L 1 norm as the performance index. This paper discuss design parameters characterizing the L 1 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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UR - http://www.scopus.com/inward/citedby.url?scp=85065295868&partnerID=8YFLogxK
M3 - Conference article
VL - 2018-October
JO - Proceedings of the International Astronautical Congress, IAC
JF - Proceedings of the International Astronautical Congress, IAC
SN - 0074-1795
ER -