Method and system for collecting air data using a laser-induced plasma channel

Patent metadata

Field	Value
Publication number	US-11828771-B2
Application number	US-201916511342-A
Country	US
Kind code	B2
Filing date	Jul 15, 2019
Priority date	Jul 15, 2019
Publication date	Nov 28, 2023
Grant date	Nov 28, 2023

Abstract

A method of measuring air data of an aircraft is provided. The method includes emitting, by a laser disposed on the aircraft, laser light into air outside the aircraft, the laser tuned to induce a laser-induced plasma channel (LIPC) in the air. The method also includes sensing, by a sensor system disposed on the aircraft, at least one property of the LIPC. The method further includes computing, by a computing device disposed on the aircraft, the air data of the aircraft based on the at least one property of the LIPC.

First claim

What is claimed is:

1. A method of measuring air data of an aircraft, the method comprising:
emitting, by a laser disposed on the aircraft, laser light toward a beam trap disposed on the aircraft, the beam trap configured to absorb the laser light, wherein the laser is tuned to induce a laser-induced plasma channel (LIPC) in air outside the aircraft between the laser and the beam trap;
sensing, by a sensor system disposed on the aircraft, an intensity of the LIPC, wherein the sensor system comprises at least one of a camera and a radar; and
computing, by a computing device disposed on the aircraft, the air data of the aircraft based on the at least one property of the LIPC, wherein said computing comprises computing an air density of air outside the aircraft, wherein said computing the air density comprises applying, by the computing device, intensity-to-density calibration data to the detected intensity to obtain the air density, and wherein the intensity-to-density calibration data corresponds to a tuning of the laser.

2. The method of claim 1 , wherein said computing the air data comprises computing, by the computing device, an airspeed of the aircraft.

3. The method of claim 1 , wherein the sensor system comprises a camera, and wherein said sensing the at least one property comprises capturing, using the camera, at least one image of the LIPC.

4. The method of claim 3 , wherein:
said capturing the at least one image comprises capturing a first image of the LIPC at a first time point and capturing a second image of the LIPC at a second time point; and
said computing the air data comprises detecting, by the computing device, a displacement of the LIPC from the first image to the second image, and computing, by the computing device, an airspeed of the aircraft based on the displacement.

5. The method of claim 3 , wherein:
said sensing the at least one property comprises detecting an intensity of the LIPC in the at least one image; and
said computing the air data comprises computing an air density of air outside the aircraft based on the intensity.

6. The method of claim 1 , wherein said emitting the laser light comprises emitting the laser light within a first frequency range, and wherein said sensing the at least one property of the LIPC comprises detecting emissions from the LIPC within a second frequency range that is non-overlapping with the first frequency range.

7. The method of claim 1 , wherein:
the sensor system comprises a first sensor disposed at a first location on the aircraft and a second sensor disposed at a second location on the aircraft, wherein the second location is offset from the first location;
said sensing the at least one property of the LIPC comprises sensing a respective position of the LIPC relative to each of the first sensor and the second sensor; and
the method further comprises estimating, by the computing device, a three-dimensional state of the aircraft based on the respective position and the offset.

8. A method of measuring air data of an aircraft, the method comprising:
emitting, by a laser disposed on the aircraft, laser light into air outside the aircraft, wherein the laser is tuned to induce a laser-induced plasma channel (LIPC) in the air;
sensing, by a sensor system disposed on the aircraft, at least one property of the LIPC, comprising:
capturing, using a camera disposed on the aircraft, at least one image of the LIPC; and
detecting an intensity of the LIPC in the at least one image; and

computing, by a computing device disposed on the aircraft, the air data of the aircraft based on the at least one property of the LIPC, comprising computing an air density of air outside the aircraft, wherein said computing the air density comprises applying, by the computing device, intensity-to-density calibration data to the detected intensity to obtain the air density, and wherein the intensity-to-density calibration data corresponds to a tuning of the laser.

9. A method of measuring air data of an aircraft, the method comprising:
emitting, by a laser disposed on the aircraft, laser light into air outside the aircraft, wherein the laser is tuned to induce a laser-induced plasma channel (LIPC) in the air;
sensing, by a sensor system disposed on the aircraft, at least one property of the LIPC; and
computing, by a computing device disposed on the aircraft, the air data of the aircraft based on the at least one property of the LIPC, wherein the sensor system comprises a radar, and wherein said sensing the at least one property of the LIPC comprises emitting, by the radar, first radio waves toward the LIPC, and receiving, by the radar, second radio waves comprising at least a portion of the first radio waves reflected by the LIPC.

10. The method of claim 9 , wherein said emitting the laser light comprises emitting the laser light toward a beam trap disposed on the aircraft, and wherein the beam trap is configured to absorb the laser light.

11. The method of claim 9 , wherein said computing the air data comprises:
detecting, by the computing device, at least one of a Doppler shift of the second radio waves or a pulse return time of the second radio waves; and
computing an airspeed of the aircraft based on the at least one of the Doppler shift or the pulse return time.

12. The method of claim 9 , wherein:
said sensing the at least one property comprises detecting an intensity of the second radio waves; and
said computing the air data comprises computing an air density of air outside the aircraft based on the intensity of the second radio waves.

13. The method of claim 12 , wherein said computing the air density comprises applying, by the computing device, intensity-to-density calibration data to the detected intensity to obtain the air density, wherein the intensity-to-density calibration data corresponds to a tuning of the laser and a tuning of the radar.

14. An air data system for measuring air data of an aircraft, the system comprising:
a laser disposed on the aircraft;
a beam trap disposed on the aircraft and configured to absorb the laser light emitted from the laser;
a sensor system disposed on the aircraft, wherein the sensor system comprises at least one of a camera and a radar; and
a computing device disposed on the aircraft and comprising at least one processor in electronic communication with the laser and the sensor system, wherein the at least one processor is configured to:
cause the laser to emit laser light into air outside the aircraft between the laser and the beam trap, wherein the laser is tuned to induce a laser-induced plasma channel (LIPC) in the air;
receive, from the sensor system, at least one property of the LIPC detected by the sensor system; and
compute the air data of the aircraft based on the at least one property of the LIPC, wherein said computing comprises computing an air density of air outside the aircraft, wherein said computing the air density comprises applying, by the computing device, intensity-to-density calibration data to the detected intensity to obtain the air density, and wherein the intensity-to-density calibration data corresponds to a tuning of the laser.

15. The air data system of claim 14 , wherein the aircraft is a rotorcraft, and wherein the laser is configured to induce the LIPC within a zone of air outside a rotor downwash zone of the rotorcraft.

16. The air data system of claim 14 , wherein the sensor system comprises a first sensor disposed at a first location on the aircraft and a second sensor disposed at a second location on the aircraft, wherein the second location is offset fr

Assignees

• Boeing Co

Inventors

• Tillotson Brian

Classifications

• G01P5/26 Primary

  by measuring the direct influence of the streaming fluid on the properties of a detecting optical wave · CPC title

• G01C23/00

  Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration · CPC title

• G01F1/7086

  using optical detecting arrangements · CPC title

• G01S17/58 Primary

  Velocity or trajectory determination systems; Sense-of-movement determination systems · CPC title

• G01S7/4808

  Evaluating distance, position or velocity data · CPC title