Method and apparatus for remote optical measurement of the position of a surface

Patent metadata

Field	Value
Publication number	US-11396385-B2
Application number	US-201916246848-A
Country	US
Kind code	B2
Filing date	Jan 14, 2019
Priority date	Jan 14, 2019
Publication date	Jul 26, 2022
Grant date	Jul 26, 2022

Abstract

Systems and methods for optically measuring a position of a measurement surface relative to a reference position. The system is a wireless network comprising a centrally located data acquisition computer and a multiplicity of remotely located sensor modules mounted at different locations within wireless communication range of a central receiver. Each sensor module is mounted to a clamp that is made specific to a control surface location and embedded with an RFID tag to denote clamp location. The optical components of the sensor modules are selected to enable indication of the linear position of a measurement surface relative to a reference position and then broadcast the measurement results. The broadcast results are received by the central receiver and processed by the data acquisition computer, which hosts human interface software that displays measurement data.

First claim

The invention claimed is:

1. A method for optically measuring a position of a measurement surface relative to a reference position, the method comprising:
(a) clamping a laser device to a reference surface so that the laser device is aimed at a measurement surface which is movable relative to the reference surface;
(b) projecting a curtain of light in a first plane from the laser device that impinges upon the measurement surface to form a laser line that includes a slice, wherein a portion of the impinging light that forms the slice of the laser line is scattered by the measurement surface toward and then impinges upon photodetectors of a row of photodetectors with an intensity that rises and falls and peaks at a center of the light from the slice of the laser line which impinges upon the photodetectors;
(c) locating an object centroid in units of pixels based on pixel data acquired by the row of photodetectors during impingement of the light from the slice of the laser line which impinges upon the photodetectors, wherein the object centroid represents a location on the row of photodetectors of peak intensity of the light from the slice of the laser line; and
(d) transmitting object centroid data signals that represent a measured position of the measurement surface relative to the reference surface.

2. The method as recited in claim 1 , wherein step (a) comprises orienting the row of photodetectors so that the row of photodetectors are aligned in a second plane that is generally perpendicular to the first plane and intersects the curtain of light.

3. The method as recited in claim 1 , wherein step (c) comprises:
finding an intensity baseline and peak;
correcting light intensity for lens vignette artifact;
interpolating pixel data for pseudo-sub-pixel resolution;
object detection thresholding; and
calculating the object centroid.

4. The method as recited in claim 1 , further comprising converting the object centroid data signals to a distance measurement using stored data representing a table or an equation that correlates pixel values with measured distances in a manner that is characteristic of relative movement of the measurement surface and reference surface.

5. The method as recited in claim 1 , wherein the reference surface is a control surface of an aircraft.

6. The method as recited in claim 5 , further comprising attaching an optical target comprising the measurement surface to a fuselage of the aircraft.

7. The method as recited in claim 1 , wherein the measurement surface is a first control surface of an aircraft.

8. The method as recited in claim 7 , wherein the reference surface is a second control surface of the aircraft.

9. The method as recited in claim 7 , wherein the reference surface is a surface of a fuselage of the aircraft.

10. The method as recited in claim 7 , wherein the reference surface is a surface of a wing of the aircraft.

11. The method as recited in claim 1 , wherein the measurement surface is a control surface of an aircraft, the method further comprising:
rotating the control surface by discrete degrees of actuation;
repeating steps (b) and (c) at each discrete degree of actuation until the measured position of the control surface relative to the reference surface is a neutral position; and
rigging operator controls to accurately reflect the neutral position of the control surface.

12. The method as recited in claim 1 , wherein the reference surface is a control surface of an aircraft, the method further comprising:
rotating the control surface by discrete degrees of actuation;
repeating steps (c) and (d) at each discrete degree of actuation until the measured position of the control surface relative to the measurement surface is a neutral position; and
rigging operator controls to accurately reflect the neutral position of the control surface.

13. A wireless network used to practice the method as recited in claim 1 , the wireless network comprising:
a computer system that hosts data acquisition software configured to convert object centroid data into distance measurement data;
a central transceiver operatively coupled to the computer system for receiving a radio-frequency signal carrying the object centroid data and transmitting the object centroid data to the computer system; and
a sensor module located within communication range of the central transceiver, wherein the sensor module comprises:
a housing;
a battery;
a laser device mounted inside the housing and configured to project a curtain of light in a first plane;
a row of photodetectors arranged in sequence along a straight line inside the housing and configured to output respective analog photodetector output signals in response to impingement of light;
a lens mounted inside the housing in front of the row of photodetectors and having a focal axis, wherein a field of view of the lens intersects the curtain of light; and wherein the focal axis of the lens and the straight line of the row of photodetectors lie in a second plane that is perpendicular to the first plane;
a microcontroller that is configured to control operation of the laser device and compute a location of an object centroid relative to the row of photodetectors based on the analog photodetector output signals output by the row of photodetectors; and
a transceiver configured to transmit a radio-frequency signal carrying object centroid data representing the location of the object centroid computed by the microcontroller,
wherein the laser device, the microcontroller and the transceiver receive electric power from the battery.

14. The wireless network as recited in claim 13 , wherein the sensor module is clamped to a surface of an aircraft.

15. The wireless network as recited in claim 13 , wherein the microcontroller is configured to control operation of the laser device to project a curtain of light in the first plane from the laser device onto a measurement surface to form an impingement line.

16. The wireless network as recited in claim 15 , wherein the microcontroller is further configured to detect an object centroid where light scattered from the impingement line impinges on the row of photodetectors.

17. The wireless network as recited in claim 16 , wherein detecting an object centroid comprises:
finding an intensity baseline and peak;
correcting light intensity for lens vignette artifact;
interpolating pixel data for pseudo-sub-pixel resolution;
object detection thresholding; and
calculating the object centroid.

18. The wireless network as recited in claim 16 , wherein the microcontroller is further configured to send object centroid data that represent a measured position of the measurement surface relative to a reference surface to the transceiver.

19. The wireless network as recited in claim 18 , wherein the computer system is configured to convert the object centroid data signals received from the transceiver to a distance measurement using stored data representing a table or an equation that correlates pixel values with measured distances in a manner that is characteristic of relative movement of the measurement surface and reference surface.

20. The wireless network as recited in claim 13 , wherein the sensor module is oriented so that the row of photodetectors are aligned in a second plane that is generally perpendicular to the first plane and intersects the curtain of light.

Assignees

• Boeing Co

Inventors

• Konyndyk David M
• Fuller Mark Douglas
• James Jerry A
• Huang Timothy P

Classifications

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B64F5/60 Primary

  Testing or inspecting aircraft components or systems · CPC title

• G01B11/26 Primary

  for measuring angles or tapers; for testing the alignment of axes · CPC title

• G01B11/026

  by measuring distance between sensor and object (G01B11/0608 takes precedence) · CPC title

• G01C15/002 Primary

  Active optical surveying means (optical plumbing G01C15/105) · CPC title