Title:
SATELLITE CONSTELLATION FORMATION SYSTEM, SATELLITE CONSTELLATION FORMATION METHOD, DEBRIS REMOVAL SCHEME, SATELLITE CONSTELLATION CONSTRUCTION SCHEME, AND GROUND EQUIPMENT
Document Type and Number:
WIPO Patent Application WO/2020/157807
Kind Code:
A1
Abstract:
A satellite constellation formation system (100) forms a satellite constellation (20). The satellite constellation (20) is composed of satellite groups (300). The satellite constellation (20) is configured such that the satellite groups (300) cooperate to provide services. The satellite constellation (20) has a plurality of orbital planes (21), each of which has a plurality of satellites (30) flying at the same orbital altitude. A satellite constellation formation unit (110) forms the satellite constellation (20) in which the orbital heights of the plurality of orbital planes (21) are different from each other.
Inventors:
MUKAE HISAYUKI (JP)
Application Number:
PCT/JP2019/002794
Publication Date:
August 06, 2020
Filing Date:
January 28, 2019
Export Citation:
Assignee:
MITSUBISHI ELECTRIC CORP (JP)
International Classes:
B64G1/10
Domestic Patent References:
| WO2017110105A1 | 2017-06-29 | |||
| WO2015190527A1 | 2015-12-17 |
Foreign References:
| JPH09130317A | 1997-05-16 | |||
| JPS6140578A | 1986-02-26 | |||
| US5979832A | 1999-11-09 | |||
| JP2016210353A | 2016-12-15 | |||
| JPH05270498A | 1993-10-19 | |||
| CN105511483A | 2016-04-20 |
Attorney, Agent or Firm:
MIZOI INTERNATIONAL PATENT FIRM (JP)
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