MULTIPLE OPERATIONAL MODES FOR AIRCRAFT LASER SENSING SYSTEMS
A system (12) for an aircraft (10) includes an optical sensor, at least one aircraft sensor, and a controller (18). The optical sensor is configured to emit a laser outside the aircraft (10), and the at least one aircraft sensor is configured to sense at least one aircraft condition. The controller...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
03.01.2024
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Subjects | |
Online Access | Get full text |
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Summary: | A system (12) for an aircraft (10) includes an optical sensor, at least one aircraft sensor, and a controller (18). The optical sensor is configured to emit a laser outside the aircraft (10), and the at least one aircraft sensor is configured to sense at least one aircraft condition. The controller (18) is configured to determine a first operational state of the aircraft (10) based upon the at least one aircraft condition and determine a second operational state of the aircraft (10) based on the at least one aircraft condition, and operate the optical sensor to emit the laser at a first intensity during the first operational state and a second intensity during the second operational state, wherein the second intensity is greater than the first intensity. |
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Bibliography: | Application Number: EP20180195405 |