CPC B64D 45/00 (2013.01) [G08G 5/0021 (2013.01); G08G 5/0039 (2013.01); H04L 45/028 (2013.01); H04L 45/60 (2013.01)] | 17 Claims |
1. A method of increasing resiliency of functionalities operating on an aircraft network system of an aircraft, the method comprising:
during inoperation of one node of a set of nodes, determining a flight condition of the aircraft;
determining a criticality of the functionalities of the aircraft that are managed by the set of nodes; and
dynamically reassigning the functionalities of the aircraft that are managed by the set of nodes;
wherein the dynamically reassigning the functionalities is based upon the criticality of the functionalities, and wherein the dynamically reassigning prioritizes higher-criticality functionalities based upon an algorithm, wherein the algorithm defines a hierarchy of criticality for the functionalities, and further dynamically changes the hierarchy of criticality for the functionalities based upon the flight condition of the aircraft.
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