Boom load alleviation using visual means

Aeronautics and astronautics – Aircraft structure – Fuel supply

Reexamination Certificate

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C244S136000

Reexamination Certificate

active

06837462

ABSTRACT:
An aircraft refueling boom load alleviation system uses received light to detect boom displacement and generates a control signal to correct the displacement. Both a set of flight surfaces and a plurality of light imageable targeting sights are disposed on a refueling tube. At least one digital camera converts the light imageable shape of each of the targeting sights to individual pixel images. The pixel images converted by the digital camera are input to a computer system. The computer system recognizes either a displacement of pixel images or a quantity change of pixels between pixel images as a displacement of the refueling tube. The computer system calculates the displacement of any of the pixel images. A signal is generated to control the refueling tube flight surfaces to correct the displacement.

REFERENCES:
patent: 5326052 (1994-07-01), Krispin et al.
patent: 5530650 (1996-06-01), Biferno et al.
patent: 6651933 (2003-11-01), von Thal et al.

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