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:
Apr. 25, 2023

Filed:

Aug. 05, 2022
Applicant:

The 28th Research Institute of China Electronics Technology Group Corporation, Nanjing, CN;

Inventors:

Xuan Wang, Nanjing, CN;

Wenyi Tang, Nanjing, CN;

Hui Ding, Nanjing, CN;

Jibo Huang, Nanjing, CN;

Yan Liu, Nanjing, CN;

Qiucheng Xu, Nanjing, CN;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 18/25 (2023.01); G06V 20/40 (2022.01); G08G 5/06 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
G06F 18/25 (2023.01); G06V 20/41 (2022.01); G08G 5/065 (2013.01); B64D 45/0005 (2013.01); B64D 2045/0085 (2013.01);
Abstract

A flight pushback state monitoring method based on multi-modal data fusion comprises: 1, constructing a control intention recognition rule, and recognizing a pushback intention from a control instruction sent by a controller; 2, constructing a flight intention recognition model, extracting an aircraft action from a real-time monitoring video, and capturing a flight intention; and 3, constructing an intention alignment fusion rule, and judging whether control intention information conflicts with flight intention information; by fusing the control intention and the flight intention, the method can realize the following auxiliary functions: timely judging whether the aircraft follows the pushback instruction sent by the controller, if a captain does not act according to the control instruction or acts arbitrarily without a control instruction, giving an inconsistent alarm, and a function of monitoring the flight pushback state is implemented.


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