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:
Aug. 28, 2018

Filed:

Nov. 17, 2016
Applicants:

Sandel Avionics, Inc., Vista, CA (US);

Priscilla Hickey;

Inventors:

Gerald J. Block, Vista, CA (US);

Jim Slattery, San Diego, CA (US);

Robert J. Bleeg, Mercer Island, WA (US);

Delmar M. Fadden, Preston, WA (US);

Richard W. Taylor, Seattle, WA (US);

Assignee:

SANDEL AVIONICS INC., Vista, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
G01C 23/00 (2006.01); B64C 13/18 (2006.01); G01C 21/20 (2006.01); B64D 43/00 (2006.01);
U.S. Cl.
CPC ...
G01C 21/20 (2013.01); B64D 43/00 (2013.01); G01C 23/00 (2013.01);
Abstract

A flight management system for controlling navigation of an aircraft includes a path guidance panel having at least one mode selector for allowing user selection of guidance mode in which the aircraft is to operate. The system also includes at least one display device having rendered thereon a navigational map. A computer module receives aircraft data from one or more aircraft components, at least one of the aircraft components being a guidance system. The computer module is configured to use information obtained from the guidance system to cause the display device to render on the navigational map a current flight plan path that is the aircraft is following.


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