According to one embodiment, an aviation system 100 includes electric field sensors 112 and a ground system 114 including a computer configured to communicate with each of the electric field sensors 112. The computer is configured to: acquire electric field intensities from the electric field sensors 112 respectively, and generate a first electric field distribution on a ground surface 16 based on the electric field intensities; derive a matrix; derive a pseudo inverse matrix of the matrix; derive an electric charge distribution on the horizontal plane by multiplying the pseudo inverse matrix by the first electric field distribution on the ground surface 16; and derive a second electric field distribution on a flight path based on the electric charge distribution. The first electric field distribution on the ground surface 16 is derived by multiplying the matrix by electric charges temporarily set on a horizontal plane at a predetermined altitude.
AVIATION SYSTEM AND AVIATION METHOD
LUFTFAHRTSYSTEM UND LUFTFAHRTVERFAHREN
SYSTÈME D'AVIATION ET PROCÉDÉ D'AVIATION
03.01.2024
Patent
Elektronische Ressource
Englisch
AVIATION LIGHTING SYSTEM, AVIATION LIGHTING CONTROL PROGRAM, AND AVIATION LIGHTING CONTROL METHOD
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