System and method for correcting wing twist of an aircraft
First Claim
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1. A system comprising:
- a first light beam locating sensor associated with a first position to be located on a wing of an aircraft;
wherein the first light beam locating sensor senses a first light beam at a first identifiable position on the first light beam locating sensor; and
a processor configured to;
receive a first signal from the first light beam locating sensor, the first signal including the first identifiable position on the first light beam locating sensor;
determine a location of the first position on the wing;
perform a first comparison of the location of the first position on the wing to a predetermined analyzed location of the first position on the wing; and
to send an instruction to control moving of a movable control surface if there is a difference in the first comparison.
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Abstract
A system which includes a first light beam locating sensor associated with a first position to be located on a wing of an aircraft. The first light beam locating sensor senses a first light beam at an identifiable position on the first light beam locating sensor. A processor is configured to receive a first signal from the first light beam locating sensor wherein the first signal includes a first identifiable position on the first light beam locating sensor. The processor is configured to determine a location of the first position on the wing and perform a first comparison of the location of the first position on the wing to a predetermined analyzed location of the first position on the wing.
17 Citations
20 Claims
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1. A system comprising:
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a first light beam locating sensor associated with a first position to be located on a wing of an aircraft;
wherein the first light beam locating sensor senses a first light beam at a first identifiable position on the first light beam locating sensor; anda processor configured to; receive a first signal from the first light beam locating sensor, the first signal including the first identifiable position on the first light beam locating sensor; determine a location of the first position on the wing; perform a first comparison of the location of the first position on the wing to a predetermined analyzed location of the first position on the wing; and to send an instruction to control moving of a movable control surface if there is a difference in the first comparison. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12)
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13. A method comprising the steps of:
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sensing a first light beam at a first identifiable position on a first light beam locating sensor, wherein the first light beam locating sensor is associated with a first position to be located on a wing of an aircraft; receiving by a processor a first signal from the first light beam locating sensor, the first signal including the first identifiable position on the first light beam locating sensor; determining by the processor a location of the first position on the wing; performing by the processor a first comparison of the location of the first position on the wing to a predetermined analyzed location of the first position on the wing; and sending by the processor a first instruction to control moving of a movable control surface if there is a difference in the first comparison. - View Dependent Claims (14, 15, 16, 17, 18, 19, 20)
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Specification