Surface condition sensing system
AssigneeHughes Aircraft Company
InventorsKurt Reiser, Scott Y. Harmon, Jennifer M. Butler
Life of this patent
Estimating the term…
Loading patent…
AssigneeHughes Aircraft Company
InventorsKurt Reiser, Scott Y. Harmon, Jennifer M. Butler
Estimating the term…
A surface condition sensing system includes a frequency controlled source of electromagnetic power adapted to produce a band of selected frequencies which are directed to a surface under examination. A monitoring circuit compares transmitted and reflected electromagnetic power as a function of frequency from the surface, and generates a plurality of absorption signals representing the difference between the amplitude of the transmitted signal with the corresponding amplitude of the reflected signal. An evaluator circuit generates a surface condition signal representing the results of a comparison between the plurality of absorption signals with known surface models. A control circuit generates a status signal representative of the surface condition. The system can be configured as a road condition sensor or as an aircraft ice detection sensor.
A surface condition sensing system comprising:
A surface condition sensing system, comprising:
An aircraft ice detection apparatus comprising:
An aircraft ice detection apparatus comprising:
A surface condition sensing system, comprising:
A surface condition sensing system, comprising:
Dependencies are inferred from the claim text.