Thermal load balancing for electronically steerable antennas
AssigneePanasonic Avionics Corporation
InventorsAnh NGUYEN, Larry GLICK
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AssigneePanasonic Avionics Corporation
InventorsAnh NGUYEN, Larry GLICK
Estimating the term…
Example embodiments disclosed herein relate to optimizing operation of an electronically steerable antenna (ESA) with respect to temperature-related constraints. Thermal load experienced by individual antenna elements or tiles of the ESA is balanced to maximize an expected time before the ESA reaches a shutdown temperature. An example method includes determining a reduced number of antenna tiles that minimally satisfies a signal quality requirement with respect to a target system. The method further includes selecting an optimized sequence of tile patterns of the reduced number of antenna tiles within the ESA. The optimized sequence corresponds to an optimized path that traverses a graph having nodes corresponding to the tile patterns and edges defining a count of shared tiles between respective tile patterns. The method further includes operating the ESA according to the optimized sequence of tile patterns based on activating specific tiles identified by each pattern in a sequential manner.
A method for an electronically steerable antenna (ESA) of a commercial passenger vehicle, the method comprising:
An antenna system for a commercial passenger vehicle, the antenna system comprising:
A non-transitory computer-readable storage medium storing executable instructions for operation of an antenna array that includes a number of antenna elements arranged adjacently, the executable instructions when executed by a processor causing the processor to:
Dependencies are inferred from the claim text.