The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 28, 2021

Filed:

Oct. 01, 2019
Applicant:

Subaru Corporation, Tokyo, JP;

Inventors:

Kumiko Kindaichi, Tokyo, JP;

Yutaka Sasaki, Tokyo, JP;

Toshiyuki Narahashi, Tokyo, JP;

Assignee:

SUBARU CORPORATION, Tokyo, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G08G 5/00 (2006.01); G01S 19/45 (2010.01); G05D 1/00 (2006.01); G01S 19/13 (2010.01); G01C 21/16 (2006.01);
U.S. Cl.
CPC ...
G08G 5/0008 (2013.01); G01C 21/165 (2013.01); G01S 19/13 (2013.01); G01S 19/45 (2013.01); G05D 1/0077 (2013.01);
Abstract

An aircraft position measurement system is provided for an aircraft configured to use an artificial satellite configured to fly in a known orbit. The aircraft position measurement system includes a reflector, a distance-angle measuring member, a satellite position obtainer, and an aircraft position calculator. The reflector configured to be mounted on the artificial satellite and reflect an electromagnetic wave in a direction in which the electromagnetic wave arrives. The distance-angle measuring member is configured to be mounted on the aircraft and emit an electromagnetic wave and measure a bearing and a distance to the artificial satellite when seen from the aircraft. The satellite position obtainer is configured to obtain an absolute position of the artificial satellite. The aircraft position calculator is configured to calculate a position of the aircraft based on the absolute position of the artificial satellite and the bearing and the distance to the artificial satellite.


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