Patent Document ID: 9932127
Application ID: 14962137
Patent Flag: 1

Claim One:
1. A method comprising: receiving, over an aircraft data communications bus, a plurality of non-pneumatic inputs corresponding to aircraft operational parameters; processing the plurality of non-pneumatic inputs through an artificial intelligence network to generate an air data output value; and outputting the air data output value to a consuming system for use when a pneumatic-based air data output value is determined to be unreliable; wherein the artificial intelligence network comprises an artificial neural network having at least one internal layer of neurons that apply one or more weights, biases, or transfer functions to each of the plurality of non-pneumatic inputs to generate the air data output value; wherein the artificial neural network is pre-trained to determine the one or more weights, biases, or transfer functions; and wherein processing the plurality of non-pneumatic inputs through the artificial intelligence network to generate the air data output value comprises processing the plurality of non-pneumatic inputs through the artificial neural network without changing the one or more weights, biases, or transfer functions.