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. 10, 2020

Filed:

Jun. 09, 2017
Applicant:

Rockwell Collins, Inc., Cedar Rapids, IA (US);

Inventors:

David A. Miller, Swisher, IA (US);

Richard M. Bradford, Cedar Rapids, IA (US);

Assignee:

Rockwell Collins, Inc., Cedar Rapids, IA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 30/15 (2020.01); H04L 29/08 (2006.01); H04L 12/24 (2006.01); H04L 12/947 (2013.01); H04Q 9/00 (2006.01); G06Q 10/06 (2012.01);
U.S. Cl.
CPC ...
G06F 30/15 (2020.01); G06Q 10/06313 (2013.01); H04L 41/08 (2013.01); H04L 49/25 (2013.01); H04L 67/12 (2013.01); H04Q 9/00 (2013.01);
Abstract

A method for optimizing the design of backplane and field bus routing for avionics network architectures determines a solution space of valid configurations defined by the intersection of universes corresponding to potential aircraft sensor locations, the data content relationships for each hosted application executing on the aircraft computing center, potential remote data concentrator (RDC) configurations, and potential backplane/field bus configurations for the avionics network architecture. The method includes identifying within the solution space, via an optimization engine, optimal configuration solutions of a desired optimality level based on connectivity constraints, system survivability constraints providing spatial separation of primary and redundant sensor and data collection systems, system robustness constraints associated with minimum functional capabilities for continued safe flight and landing capability, and an objective function characterizing overall desirability.


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