Title:
SATELLITE CONTROL METHOD
Document Type and Number:
WIPO Patent Application WO/2023/149386
Kind Code:
A1
Abstract:
Provided is a satellite control method capable of suppressing cost for purchasing, remanufacturing, operating, and the like, of an artificial satellite. A satellite control method according to the present invention comprises: a separation step for separating, from a platform satellite P that revolves while being joined together with a first mission satellite M1 along a first orbit and that supplies the first mission satellite with electric power for enabling the first mission satellite to execute a mission on a stationery orbit, the first mission satellite M1; a joining step for joining a second mission satellite M2 injected into the first orbit with the platform satellite P; and a post-joining step for causing the platform satellite P joined with the second mission satellite M2 to revolve along the first orbit or to move along another orbit different from the first orbit.
Inventors:
TANAKA ATSUSHI (JP)
Application Number:
PCT/JP2023/002763
Publication Date:
August 10, 2023
Filing Date:
January 29, 2023
Export Citation:
Assignee:
SKYDEER CORP (JP)
International Classes:
B64G1/10; B64G1/24; B64G1/26; B64G1/42; B64G1/62; B64G1/64
Foreign References:
| US20170029138A1 | 2017-02-02 | |||
| JPH08244693A | 1996-09-24 | |||
| JP2018171947A | 2018-11-08 | |||
| JPS58142000A | 1983-08-23 | |||
| JP2021049907A | 2021-04-01 | |||
| US20030029969A1 | 2003-02-13 |
Attorney, Agent or Firm:
YAMASHIRO Naoki (JP)
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