Title:
SATELLITE POSITION/ATTITUDE CONTROL SYSTEM, AND SATELLITE POSITION/ATTITUDE CONTROL METHOD
Document Type and Number:
WIPO Patent Application WO/2020/045180
Kind Code:
A1
Abstract:
[Problem] To control relative positions and attitudes of artificial satellites by magnetic force alone without limiting the use to the orbit of celestial bodies where geomagnetism exists. [Solution] A satellite position/attitude control system 1 for controlling relative positions and attitudes of a master satellite 2 and a slave satellite 3, wherein the master satellite 2 and the slave satellite 3 each have a triaxial magnetic field generation sources 21, 31 and control units 24, 34, and the control units 24, 34 control the magnetic flux density vector of the magnetic field generated by the triaxial magnetic field generation sources 21, 31 according to the relative positions and attitudes of the master satellite 2 and the slave satellite 3.
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Inventors:
NODA ATSUSHI (JP)
SHIRASAWA YOJI (JP)
SHIGETO SHUHEI (JP)
SHIBATA YUICHI (JP)
HASHIMOTO SHINTARO (JP)
TSUCHIYA NAOHIRO (JP)
SHIRASAWA YOJI (JP)
SHIGETO SHUHEI (JP)
SHIBATA YUICHI (JP)
HASHIMOTO SHINTARO (JP)
TSUCHIYA NAOHIRO (JP)
Application Number:
PCT/JP2019/032595
Publication Date:
March 05, 2020
Filing Date:
August 21, 2019
Export Citation:
Assignee:
JAPAN AEROSPACE EXPLORATION (JP)
International Classes:
B64G1/24; G05D1/08
Foreign References:
| US20070295865A1 | 2007-12-27 | |||
| CN108628345A | 2018-10-09 | |||
| US6089510A | 2000-07-18 | |||
| US20030098394A1 | 2003-05-29 | |||
| JP2003212197A | 2003-07-30 | |||
| CN106094854A | 2016-11-09 |
Attorney, Agent or Firm:
OMORI, Junichi (JP)
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