Granted Patent B2

US 12,625,272 · App. 17/922,929 · Granted May 12, 2026

Inventors: David Tomline Michel (Orsay, FR); Laurent Mugnier (Meudon, FR); Matthieu Valla (Epinay sur Orge, FR)

Assignee: OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AÉROSPATIALES

G01S17/95G01S7/4865G01S7/4917G01S17/58

Abstract

Claims (51)

1 . A detection and telemetry process using electromagnetic radiation pulses, in order to characterize a radial velocity distribution as a function of a separation distance within an exploration zone, comprising the following steps:

1) getting a system for detection and telemetry by using electromagnetic radiation pulses, that is adapted for, during an acquisition sequence, emitting at least one electromagnetic radiation pulse, detecting a portion of said at least one radiation pulse which was backscattered by at least one target present in the exploration zone, and producing a measurement signal which corresponds to the backscattered and detected radiation pulse portion, where said measurement signal contains information on a separation distance and a radial velocity of each target, the information on the radial velocity of each target corresponds to a frequency shift due to a Doppler effect which occurs when the radiation is backscattered by this target; and

2) performing an acquisition sequence by controlling the system for emitting the at least one pulse into the exploration,

wherein the process further comprises the following additional steps:

3) getting a characterization of an impulse response of the system, where the impulse response corresponds to the measurement signal which is produced by said system during an acquisition sequence and when a single backscattering element is in the exploration zone, said single backscattering element corresponding to a single separation distance value and having a known radial velocity value relative to the system, and when the exploration zone has no backscattering element other than the so-called single backscattering element; and

4) by treating the measurement signal which was produced in step 2) as a sum of contributions which each correspond to the impulse response applied to a value for the separation distance and to a value for the radial velocity, and multiplied by a backscattering amplitude value, getting by decomposition of the measurement signal into several contributions, a measurement result in a form of pairs which are each comprised of a backscattering amplitude value and a radial velocity value, and which are assigned respectively to several separation distance values within the exploration zone.

2 . The process according to claim 1 , wherein the impulse response is a function of both the separation distance, or round-trip time of the radiation from an optical outlet of the system, and also of one among:

a spectral component frequency of the radiation pulse portion which was backscattered and then detected by the system;

a frequency shift between a spectral component of the radiation pulse portion

which was backscattered and then detected by the system, and the radiation of each pulse as emitted by said system, or a radial velocity value associated with said frequency shift by the Doppler effect; and

a frequency of a spectrum of the measurement signal which is used in step 3).

3 . The process according to claim 1 , wherein the characterization of the impulse response is obtained in step 3) by performing at least one acquisition sequence with the detection and telemetry system by using electromagnetic radiation pulses, and with a single backscattering element which is positioned at a determined separation distance in the exploration zone,

or by performing a numerical simulation of operation of the system when a single backscattering element is present at a determined separation distance in the exploration zone.

4 . The process according to claim 1 , wherein the detection and telemetry system by using electromagnetic radiation pulses is adapted for implementing a heterodyne detection mode, and the measurement signal which is produced at each acquisition sequence and which is used in step 4), is a heterodyne measurement signal.

5 . The process according to claim 1 , wherein the detection and telemetry system by using electromagnetic radiation pulses is of LIDAR type and the radiation of each pulse emitted by said system is a laser radiation, or

the detection and telemetry system by using electromagnetic radiation pulses is of RADAR type and the radiation of each pulse emitted by said system has a vacuum wavelength comprised between 1 mm and 7.5 mm.

6 . The process according to claim 5 , wherein the detection and telemetry system by using electromagnetic radiation pulses is of LIDAR type, and wherein each radiation pulse has at least one of the following features:

a radiation wavelength inside the pulse is comprised between 250 nm and 10 μm;

a duration of the pulse is comprised between 50 ns and 1 μs; and

the pulse has a frequency width at half-maximum which is less than 1 GHz.

7 . The process according to claim 1 , wherein the measurement result is deduced from the measurement signal in step 4) by applying a two-dimensional decomposition algorithm which uses a method selected in the list comprising a a-posteriori maximum method, a maximum likelihood method, and a stochastic method.

8 . The process according to claim 7 , further comprising an additional step which is executed from the measurement result provided by the two-dimensional decomposition algorithm, in order to reduce widths of radial velocity distributions which are separately assigned to several values of the separation distance in the exploration zone.

9 . The process according to claim 1 , wherein step 4) includes assigning a single radial velocity value and a single backscattered amplitude value to each value of the separation distance, for a sampling of values of the separation distance inside the exploration zone, and then calculating a reconstruction of the measurement signal as a sum of contributions each equal to the impulse response applied to a separation distance value and to the radial velocity value which was assigned to said separation distance value, and multiplied by the backscattered amplitude value which was also assigned to the same separation distance value, for all the separation distance values in the sampling, and then performing a series of iterative adjustments of the assigned radial velocity and backscattered amplitude values, so as to reduce a deviation between the measurement signal which was produced in step 2) and the reconstruction of the measurement signal resulting from the values assigned to the radial velocity and backscattered amplitude,

wherein the measurement result is then formed by the radial velocity and backscattered amplitude values assigned to the separation distance values, which provide a minimum deviation between the measurement signal and the reconstruction of the measurement signal.

10 . The process according to claim 1 , used for at least one of the following applications:

meteorological measurements;

measurements of diffusion of atmospheric pollutants;

measurements of local concentration of backscattering particles suspended in an environment, or of chemical compounds which absorb and re-emit the radiation of the pulses;

measurements of shearing of an atmospheric flow;

measurements of position and/or lifetime of at least one vortex which is present in a fluid flow;

anemometric measurements which are performed from an aircraft in flight;

anemometric measurements which are performed to optimize operation of a wind turbine; and

anemometrical measurements which are performed for adjusting aircraft flight in formation, or for adjusting a drone flight.

11 . The process according to claim 2 , wherein the characterization of the impulse

response is obtained in step 3) by performing at least one acquisition sequence with the detection and telemetry system by using electromagnetic radiation pulses, and with a single backscattering element which is positioned at a determined separation distance in the exploration zone,

or by performing a numerical simulation of operation of the system when a single backscattering element is present at a determined separation distance in the exploration zone.

12 . The process according to claim 2 , wherein the detection and telemetry system by

using electromagnetic radiation pulses is adapted for implementing a heterodyne detection mode, and the measurement signal which is produced at each acquisition sequence and which is used in step 4), is a heterodyne measurement signal.

13 . The process according to claim 3 , wherein the detection and telemetry system by

using electromagnetic radiation pulses is adapted for implementing a heterodyne detection mode, and the measurement signal which is produced at each acquisition sequence and which is used in step 4), is a heterodyne measurement signal.

14 . The process according to claim 2 , wherein the detection and telemetry system by

using electromagnetic radiation pulses is of LID AR type and the radiation of each pulse emitted by said system is a laser radiation, or

the detection and telemetry system by using electromagnetic radiation pulses is of RADAR type and the radiation of each pulse emitted by said system has a vacuum wavelength comprised between 1 mm and 7.5 mm.

15 . The process according to claim 3 , wherein the detection and telemetry system by

using electromagnetic radiation pulses is of LID AR type and the radiation of each pulse emitted by said system is a laser radiation, or

the detection and telemetry system by using electromagnetic radiation pulses is of RADAR type and the radiation of each pulse emitted by said system has a vacuum wavelength comprised between 1 mm and 7.5 mm.

16 . The process according to claim 4 , wherein the detection and telemetry system by

using electromagnetic radiation pulses is of LID AR type and the radiation of each pulse emitted by said system is a laser radiation, or

the detection and telemetry system by using electromagnetic radiation pulses is of RADAR type and the radiation of each pulse emitted by said system has a vacuum wavelength comprised between 1 mm and 7.5 mm.

17 . The process according to claim 2 , wherein the measurement result is deduced from the measurement signal in step 4) by applying a two-dimensional decomposition algorithm which uses a method selected in the list comprising a a-posteriori maximum method, a maximum likelihood method, and a stochastic method.

18 . The process according to claim 3 , wherein the measurement result is deduced from the measurement signal in step 4) by applying a two-dimensional decomposition algorithm which uses a method selected in the list comprising a a-posteriori maximum method, a maximum likelihood method, and a stochastic method.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (29)