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:
Nov. 07, 2023

Filed:

Oct. 05, 2020
Applicant:

Zipline International Inc., South San Francisco, CA (US);

Inventors:

Peter Abeles, Redwood City, CA (US);

Keenan Wyrobek, Half Moon Bay, CA (US);

Assignee:

Zipline International Inc., South San Francisco, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 39/02 (2023.01); G06T 7/73 (2017.01); B64F 5/60 (2017.01); B64U 70/00 (2023.01); B64U 80/00 (2023.01);
U.S. Cl.
CPC ...
B64C 39/024 (2013.01); B64F 5/60 (2017.01); G06T 7/73 (2017.01); B64U 70/00 (2023.01); B64U 80/00 (2023.01); B64U 2201/20 (2023.01); G06T 2207/30204 (2013.01); G06T 2207/30252 (2013.01);
Abstract

A system includes a camera configured such that a field of view of the camera is positioned to capture a base portion and a movable portion of an aircraft. A computer communicatively connected to the camera is configured to determine a relative orientation between a base identification feature of the base portion and a movable identification feature of the movable portion of the aircraft based on image data received from the camera. The computer is also configured to determine a position of the movable portion of the aircraft based on the relative orientation between the base identification feature and the movable identification feature and a position of the base portion and to compare the position of the movable portion to a reported position for the movable portion to determine a variance. An aircraft control system is configured to monitor a state of the aircraft based on the variance.


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