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:
Dec. 31, 2024

Filed:

Sep. 01, 2020
Applicant:

Mitsubishi Heavy Industries, Ltd., Tokyo, JP;

Inventor:

Toru Kojima, Tokyo, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 45/08 (2006.01); B64F 1/02 (2006.01); B64U 20/87 (2023.01); B64U 70/30 (2023.01); B64U 70/92 (2023.01); G05D 1/00 (2006.01); B64U 101/30 (2023.01);
U.S. Cl.
CPC ...
G05D 1/101 (2013.01); B64D 45/08 (2013.01); B64U 20/87 (2023.01); B64U 70/30 (2023.01); B64U 70/92 (2023.01); B64F 1/02 (2013.01); B64U 2101/30 (2023.01);
Abstract

An aircraft position control system includes a processor configured to calculate a feedback manipulated variable of an aircraft by feedback control so that the aircraft heads toward a target landing point, based on at least a relative position and a relative velocity. The processor is further configured to set an addition value, by referring to a switching line preliminarily provided in a manner passing through an origin of a coordinate plane having orthogonal axes representing the relative position and the relative velocity and separating an acceleration region in which the relative velocity is to be increased and a deceleration region in which the relative velocity is to be decreased. The addition value tends to increase the relative velocity when a coordinate point of a current relative position and a current relative velocity is located in the acceleration region to calculate a manipulated variable of the aircraft.


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