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WO2024039845A1 - Capteur de vent et procédé de fabrication d'estimations de direction de vent et de vitesse de vent - Google Patents

Capteur de vent et procédé de fabrication d'estimations de direction de vent et de vitesse de vent Download PDF

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Publication number
WO2024039845A1
WO2024039845A1 PCT/US2023/030575 US2023030575W WO2024039845A1 WO 2024039845 A1 WO2024039845 A1 WO 2024039845A1 US 2023030575 W US2023030575 W US 2023030575W WO 2024039845 A1 WO2024039845 A1 WO 2024039845A1
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WO
WIPO (PCT)
Prior art keywords
wind
shell body
spherical shell
pressure
sensor
Prior art date
Application number
PCT/US2023/030575
Other languages
English (en)
Inventor
Behdad DAVOUDI
Ella ATKINS
Original Assignee
The Regents Of The University Of Michigan
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by The Regents Of The University Of Michigan filed Critical The Regents Of The University Of Michigan
Publication of WO2024039845A1 publication Critical patent/WO2024039845A1/fr

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00—Indicating or recording presence, absence, or direction, of movement
    • G01P13/02—Indicating direction only, e.g. by weather vane
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01W—METEOROLOGY
    • G01W1/00—Meteorology
    • G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06N—COMPUTING ARRANGEMENTS BASED ON SPECIFIC COMPUTATIONAL MODELS
    • G06N3/00—Computing arrangements based on biological models
    • G06N3/02—Neural networks
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P21/00—Testing or calibrating of apparatus or devices covered by the preceding groups
    • G01P21/02—Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers
    • G01P21/025—Testing or calibrating of apparatus or devices covered by the preceding groups of speedometers for measuring speed of fluids; for measuring speed of bodies relative to fluids

Definitions

  • This disclosure relates generally to wind sensors and, more particularly, relates to making wind direction and wind velocity estimations.
  • Wind sensors measure wind direction and wind velocity, and are employed in a multitude of applications. Wind sensors and their measurements are useful in controlling navigation of unmanned aerial vehicles (UAVs), for instance, amid autonomous, semi- autonomous, and other operational modes, and especially when sudden and strong wind gusts are encountered during flight. Other specific applications include fume tracking for chemical and biological defense purposes, and anemotaxis as a key component of chemotaxis. Still, more generally, wind sensors may find ready employment in self-driving cars, wind farms, marine applications, and stationary weather stations, among many other possibilities. Past wind sensors have proved too large and/or too heavy for certain installations sensitive to size and weight and subject to packaging demands, or have lacked the fidelity often needed for the particular application.
  • a wind sensor may include a spherical shell body, a multitude of pressure taps, and a multitude of pressure transducers.
  • the pressure taps are coupled with the spherical shell body.
  • the pressure taps fluidly communicate with an exterior of the spherical shell body.
  • the pressure taps have varying and differing locations relative to one another at the spherical shell body, and more particularly at the exterior of the spherical shell body.
  • the pressure transducers have connections with the pressure taps.
  • a method and process of making wind direction and wind velocity estimations may involve various steps. In one step, pressure measurements are taken at. a multitude of locations on a spherical shell body. In another step, the pressure measurements are utilized in an inverse mathematical model. In yet another step, the inverse mathematical model is developed with machine learning. And in another step, the wind direction and wind velocity estimations are made by way of the inverse mathematical model.
  • a wind sensor may include a spherical shell body, a multitude of pressure taps, and a multitude of pressure transducers.
  • the spherical shell body has an exterior wall.
  • a multitude of openings resides in the exterior wall.
  • the openings fluidly communicate with an exterior outside of the spherical shell body.
  • the openings have different locations at the exterior wall with respect to one another.
  • the pressure taps have a multitude of tubes.
  • the tubes extend to the openings.
  • the tubes fluidly communicate with the openings.
  • the pressure transducers have connections with the pressure taps by way of the tubes.
  • FIG. 1 is a perspective view of an embodiment of a wind sensor
  • FIG. 2 is a front view' of the wind sensor
  • FIG. 3 is a top view of the wind sensor
  • FIG. 4 is a flow chart of an embodiment of a method of making wind direction and wind velocity estimations
  • FIG. 5 illustrates another embodiment of the wind sensor
  • FIG. 6 presents a graph of a simulation demonstrating pressure coefficient distribution over a sphere for various velocities, with positions (xZD) relative to the sphere plotted on an x- axis and pressure coefficient (Cp) plotted on a y-axis;
  • FIG. 7 presents a graph of a simulation demonstrating machine learning results for error for pitch (0) angles of estimations of degrees ranging between -45° and +45° (i.e., -45° ⁇ ⁇ ⁇ 45°), with machine learning incidents plotted on a y-axis and with error in pitch (0) angle estimation plotted on an x-axis;
  • FIG. 8 presents a graph of a simulation demonstrating machine learning results for error in speed (meters per second, m/s) of estimations, with machine learning incidents plotted on a y-axis and with error in speed estimation plotted on an x-axis; and
  • FIG. 9 presents a graph of a simulation demonstrating machine learning results for error in azimuth ( ⁇ ) angles of estimations of degrees ranging between 0° and 360° (i.e., 0° ⁇ ⁇ 360°), with predictions plotted on a y-axis and truth plotted on an x-axis.
  • FIG. 10 An embodiment of a wind sensor 10 is presented, as well as an embodiment of a method 100 of making wind flow direction and wind flow velocity (i.e., magnitude) estimations and predictions.
  • the wind sensor 10 employs certain fundamentals of aerodynamics and machine learning capabilities in order to make wind condition estimations.
  • the wind sensor 10 is designed and constructed with size, weight, power, and cost (SWaP-C) optimizations — the wind sensor 10 possesses minimized size and packaging, and is lightweight, readying the wind sensor 10 for installations sensitive to these properties.
  • SWaP-C size, weight, power, and cost
  • the wind sensor 10 exhibits enhanced fidelity compared to past devices of comparable size and weight, and the wind sensor 10 can make wind condition estimations in three dimensions (i.e., U, V, and W) about its exterior. Furthermore, the wind sensor 10 has no moving parts which have proven prone to damage and dysfunction in severe weather conditions in past devices.
  • the wind sensor 10 and method 100 described herein have expansive applications and purposes including, but not limited to, civilian, commercial, military, recreational, and agricultural applications, and for use in UAV navigation control, fume tracking, anemotaxis, self-driving cars, wind farms, marine applications, and stationary weather stations, among many other possibilities.
  • the wind sensor 10 and method 100 can be employed for more precise pesticide spraying procedures, as well as other agricultural chemical and solution spraying procedures.
  • the wind sensor 10 could be mounted on a UAV to estimate wind condition for predicting the trajectory of dispensed chemicals and solutions for ensuring intended targeting.
  • Another application of the wind sensor 10 and method 100 can involve recreation vehicles (RVs), commercial semi-trailer trucks, and other large vehicles.
  • RVs recreation vehicles
  • commercial semi-trailer trucks and other large vehicles.
  • the wind sensor 10 and method 100 could be employed for monitoring crosswind magnitudes amid travel and the detection of strong crosswinds that may pose risk of a rollover or some other unwanted event.
  • the wind sensor 10 and method 100 could be part of a larger system that controls vehicle speed based in part or more upon wind conditions in order to optimize fuel efficiency of the particular vehicle; here, estimated wind flow directions and velocities could be an input to the larger system for vehicle speed control and adjustments with respect to estimated wind conditions.
  • the wind sensor 10 and method 100 of making wind flow direction and wind flow velocity estimations and predictions can vary in different embodiments depending upon, among other potential factors, the desired accuracy of the wind condition estimations and predictions and the intended installation and application. It will become apparent to skilled artisans as this description advances that the wind sensor 10 could have more, less, and/or different components than those set forth with reference to the figures and described herein, and that the method 100 could have more, less, and/or different steps than those depicted in FIG. 4 and described herein. With reference to FIGS. 1 -3, this embodiment of the wind sensor 10 includes a spherical shell body 12, a stem 14, a multitude of pressure taps 16, a multitude of pressure transducers 18, and a controller 20.
  • the spherical shell body 12 houses the pressure taps 16 and is exposed to surrounding wind conditions in application and amid use of the wind sensor 10 in order for the pressure taps 16 to accept the attendant wind flow of the surrounding wind conditions.
  • the attendant wind flow facilitates wind pressure readings and measurements via the pressure taps 16 and pressure transducers 18.
  • the spherical shell body 12 has an approximate two-inch (2") diameter, and in another example the diameter of the spherical shell body 12 ranges from half an meh to three inches (0.5"--3.0"); still, the spherical shell body 12 can have other dimensions in other embodiments, some smaller and some larger than these examples.
  • the spherical shell body 12 Since the spherical shell body 12 possesses a spherical and globe-like shape, wind can more readily flow around the shape, it has been found, enhancing fidelity of the wind pressure readings and measurements and minimizing or altogether precluding reading errors.
  • the spherical shape facilitates wind pressure readings and measurements in three dimensions (i.e., U, V, and W) about an exterior E of the spherical shell body 12 — for example, wind pressure readings and measurements encountered by the spherical shell body 12 horizontally and vertically relative thereto, as well as in other directions, can be readily gauged.
  • the spherical shell body 12 has an exterior wall 22.
  • the exterior wall 22 establishes and defines a hollow interior I of the spherical shell body 12.
  • the exterior wall 22 can be composed of a plastic material, a metal material, or some other material, per varying embodiments.
  • the spherical shell body 12 could also house and carry the pressure transducers 18 and the controller 20 within the interior I.
  • the stem 14 extends to the spherical shell body 12 and serves as an upright to support positioning of the spherical shell body 12 in installation.
  • the pressure taps 16 and its tubes are received in the stem 14 and are routed to the pressure transducers 18 by way of the stem’s interior, per this embodiment; still, in the embodiment in which the pressure transducers 18 and controller 20 are housed in the spherical shell body 12, the tubes would not be received and routed in the stem 14.
  • the stem 14 can be tubular. In this embodiment, the stem 14 extends wholly through the interior I of the spherical shell body 12 from a bottom side and to a topside thereof (bottom and top are used here with reference to the orientation presented by FIG.
  • the stem 14 need not extend wholly through the interior I and could instead exhibit an external mounting to the exterior wall 22.
  • a wall 24 of the stem 14 can have throughways residing in its structure to receive the pressure taps 16 and its tubes. The pressure taps 16 and its tubes pass through the throughways.
  • the wall 24 can be composed of a plastic material, a metal material, or some other material, per varying embodiments.
  • the pressure taps 16 are coupled with the spherical shell body 12 and serve to gauge static surface and wind pressures at their respective locations and sites.
  • the pressure taps 16 fluidly communicate with the exterior E of the spherical shell body 12, and have connections with the pressure transducers 18 via the fluid communication.
  • the pressure taps 16 accept surrounding wind flow at their respective sites at the exterior wall 22.
  • the quantity of pressure taps 16 can differ in varying embodiments, and can be dictated by the size of the spherical shell body 12 and the desired accuracy of the wind condition estimations and predictions. In general, it has been found that the greater the number of pressure taps 16 provided for the wind sensor 10, the greater the precision and accuracy of the wind condition estimations and predictions. In the embodiment of FIGS.
  • Openings 25 defined in and residing in the exterior wall 22 effect fluid communication between the pressure taps 16 and the exterior E, and are open to and fluidly communicate therewith. Except for the openings 25, the exterior wall 22 of the spherical shell body 12 is otherwise a substantially solid structure.
  • the pressure taps 16 extend from these openings 25.
  • the openings 25 have immediate and direct exposure to the exterior E. The sizes and shapes of the openings 25 can complement those of the pressure taps 16 at interfaces thereamong, and can be configured to facilitate fluid communication thereamong.
  • the openings 25 have an approximate diameter of 0.34 millimeters (mm) or less; still, the openings 25 can have other diameter values in other embodiments, some larger than this example. It has been found that, according to certa in embodiments, having diameters of the openings 25 less than approximately 0.34 mm can facilitate wind flow measurements by the wind sensor 10.
  • the pressure taps 16 include tubes 26 that span from the openings 25 and through the interior I of the spherical shell body 12. The tubes 26 fluidly communicate with the openings 25, and extend to the pressure transducers 18.
  • the pressure taps 16 can have coupling locations and sites at the exterior wall 22 that differ with respect to one another.
  • the locations and sites can be configured in order to facilitate wind pressure readings and measurements in three dimensions about the exterior E of the spherical shell body 12.
  • the locations and sites can be equally and symmetrically spaced around the exterior wall 22 with respect to one another, as an example.
  • a first pressure tap can have a first location at the exterior wall 22
  • a second pressure tap can have a second location at the exterior wall 22
  • a third pressure tap can have a third location at the exterior wall 22
  • a fourth pressure tap can have a fourth location at the exterior wall 22
  • a fifth pressure tap can have a fifth location at the exterior wail 22
  • a sixth pressure tap can have a sixth location at the exterior wall 22.
  • the first location and second location can be set approximately one-hundred-and-eighty- degrees (180°) from each other relative to the spherical shell body 12
  • the third location and fourth location can be set approximately one-hundred-and-eighty-degrees (180°) from each other relative to the spherical shell body 12
  • the fifth location and sixth location can be set approximately one-hundred-and-eighty-degrees (180°) from each other relative to the spherical shell body 12.
  • first and second locations can be set approximately ninety degrees (90°) from the third and fourth locations relative to the spherical shell body 12 and the third and fourth locations can be set approximately ninety degrees (90°) from the fifth and sixth locations relative to the spherical shell body 12,
  • the individual pressure taps are arranged uniformly about the spherical shell body 12, and ninety degrees (90°) from one another. Still, many other locations and sites are possible, including those that do not necessarily exhibit an equidistant and symmetrical arrangement.
  • the pressure transducers 18 have connections with the pressure taps 16 and receive wind pressure readings and measurements therefrom for conversion to electrical output signals to the controller 20. Together, the pressure transducers 18 and pressure taps 16 serve to measure surface pressure at an exterior surface of the exterior wall 22 exposed to surrounding and outside wind conditions. The connections can be via ports of the pressure transducers 18, as an example. The electrical output signals are representative of the wind pressure readings and measurements.
  • the pressure transducers 18 electrically communicate with the controller 20. While only a single pressure transducer 18 is depicted in FIG. 1 in schematic representation, there may be multiple pressure transducers 18 per varying embodiments such as one pressure transducer 18 for each pressure tap 16.
  • the pressure transducers 18 are in the form of miniature amplified output pressure sensors supplied by the Amphenol All Sensors Company of California, U.S.A. (www.allsensors.com) and under the part number 1 INCH-D1-4V-MINI; still, in other embodiments other types and kinds of pressure transducers supplied by other companies can be used.
  • the controller 20 receives the electrical output signals from the pressure transducers 18 and employs an inverse mathematical model and machine learning in order to estimate the wind flow' directions and wind flow- velocities at the spherical shell body 12 amid use of the wind sensor 10.
  • the controller 20 can be a component of an assemblage that includes the wind sensor 10, or can be a component of a larger application assemblage such as a UAV component.
  • the controller 20 when the controller 20 is a component of the wind sensor 10, the controller 20 could be housed in the spherical shell body 12 and carried thereby for a compact configuration.
  • the controller 20 can be a microcontroller, per various embodiments.
  • the inverse mathematical model serves to yield wind flow direction and wind flow velocity estimations and predictions of the wind that acts on the wind sensor 10 at the spherical shell body 12.
  • the inverse mathematical model is developed by machine learning capabilities, per below.
  • the estimations and predictions are based on the wind pressure readings and measurements of the pressure taps 16, and the distribution of the wind pressure readings and measurements around the spherical shell body 12 at the various coupling locations and sites of the pressure taps 16.
  • the wind pressures constitute model parameters of the inverse mathematical model.
  • the inverse mathematical model utilizes certain aerodynamic properties of the wind flow around the spherical shell body 12 in its estimations of wind flow directions and velocities.
  • the aerodynamic properties can include, but are not limited to, one or more of: pressure coefficient distribution around the spherical shell body 12, Reynolds number, angle at which the boundary layer separates, location of stagnation point, and air density.
  • Machine learning capabilities are used to develop the inverse mathematical model for the estimations and predictions of the wind flow directions and wind flow velocities amid use of the wind sensor 10.
  • the machine learning capabilities are incorporated with the inverse mathematical model.
  • the machine learning can involve neural networks, per an embodiment.
  • the machine learning capabilities can establish a relationship between the wind pressure readings and measurements of the pressure taps 16, and the distribution of the wind pressure readings and measurements around the spherical shell body 12 at the various coupling locations and sites of the pressure taps 16, and wind flow direction and wind flow velocities, in order to perform the estimations and predictions. Training was conducted for the machine- learning enabled inverse mathematical model offline and pre-installation for calibration purposes of the model.
  • CFD Computational fluid dynamics
  • the method 100 of making wind flow direction and wind flow velocity estimations and predictions can involve differing steps according to varying embodiments and performed in varying sequences and orders.
  • the method 100 includes a first step 110 of taking pressure readings and measurements at a multitude of locations on the spherical shell body 12 of the wind sensor 10.
  • a second step 120 involves using the pressure readings and measurements in the inverse mathematical model.
  • a third step 130 involves developing the inverse mathematical model with machine learning in order to make the wind flow direction and wind flow velocity estimations and predictions.
  • a fourth step 140 involves making the wind direction and wind velocity estimations by way of the developed inverse mathematical model.
  • other steps of the method 100 may include using pressure distribution of the pressure readings and measurements in the inverse mathematical model, making wind condition estimations in three dimensions, and/or using neural networks to develop the inverse mathematical model.
  • parameters and specifications of the wind sensor 10 and its components may be dictated by the intended application and the expected wind conditions subject to estimation and prediction.
  • pressure taps and transducers could be selected on the basis of experiencing maximum wind flow velocities of thirty miles-per-hour (30 mph) to 50 mph, or more; in large vehicle applications such as semi-trailer trucks, pressure taps and transducers could be selected on the basis of experiencing maximum wind flow velocities of 140 mph, or more; and in military chemical defense applications, the pressure taps and transducers could be selected on the basis of experiencing maximum wind flow velocities of 10 mph, or more.
  • the wind sensor 10 could have other designs, constructions, and components according to other embodiments.
  • the wind sensor 10 could be equipped with a humidity sensor and/or a temperature sensor.
  • the wind flow direction and wind flow velocity estimations and predictions could be outputted and communicated to user or operator devices or elsewhere via wired communications or wireless communications (e.g., Wi-Fi, Bluetooth) for further use.
  • FIG. 5 a second embodiment of a wind sensor 210 is presented.
  • the wind sensor is indicated by numeral 10 in the first embodiment, and is correspondingly indicated by numeral 210 in the second embodiment.
  • similarities may exist between the first embodiment and the second embodiment, some of which may not be repeated here in the description of the second embodiment.
  • the wind sensor 210 of FIG. 5 includes a spherical shell body 212, a multitude of pressure taps 216, a multitude of pressure transducers 218, and a controller 220.
  • An exterior wall 222 of the spherical shell body 212 establishes and defines a hollow interior I.
  • the spherical shell body 212 houses other components of the wind sensor 210 at its interior I. It has been found that, in certain applications and uses, locating components inside the spherical shell body 212 — and lacking components at the exterior and outside of the spherical shell body 212 — provides more efficient and effective overall packaging of the wind sensor 210, and provides increased robustness in performance.
  • the pressure taps 216, pressure transducers 218, and controller 220 are all located and positioned within the interior I of the spherical shell body 212. Further, while only three pressure taps 216 are shown in the view of FIG. 5, a total of six pressure taps 216 are provided in the second embodiment (i.e., three pressure taps 216 are unshown and hidden by a circuit board and are located at an opposite side of spherical shell body 212).
  • the pressure taps 216 each include a tube 226 that are wholly confined within the interior I of the spherical shell body 212. As before, the tubes 226 fluidly communicate with openings 225 residing in the exterior wall 222.
  • the openings 225 are depicted by an exaggerated size for demonstrative purposes in the figure.
  • the pressure transducers 218 are wholly confined within the interior I of the spherical shell body 212. Three pressure transducers 218 are shown for each of the three pressure taps 216 shown. Three more pressure transducers 218 for the three unshown pressure taps 216 are provided in this embodiment.
  • the pressure transducers 218 are mounted to and carried by a circuit board 221,
  • the circuit board 221 is also wholly confined within the interior I of the spherical shell body 212.
  • the controller 220 is a microcontroller in the second embodiment, and is carried at the circuit board 221.
  • FIGS. 7-9 demonstrate the efficacy and general precision of the machine learning capabilities for the estimations and predictions of the wind flow directions and wind flow velocities amid use of the wind sensor 10, 210.
  • Machine learning results involving neural networks are presented in graphical form in FIGS. 7-9. In FIG.
  • machine learning results for error for pitch ( ⁇ ) angles of estimations of degrees ranging between -45° and +45° are shown.
  • Machine learning incidents are plotted on a y-axis in the graph of FIG. 7, and error in pitch (0) angle estimation is plotted on an x-axis.
  • the numeral zero (0) on the x-axis represents the absence of error.
  • machine learning results for error in speed (meters per second, m/s) of estimations are shown.
  • Machine learning incidents are plotted on a y-axis in the graph of FIG. 8, and error in speed estimation is plotted on an x-axis.
  • the terms “general” and “generally” and “substantially” are intended to account for the inherent degree of variance and imprecision that is often attributed to, and often accompanies, any design and manufacturing process, including engineering tolerances — and without deviation from the relevant functionality and intended outcome — such that mathematical precision and exactitude is not implied and, in some instances, is not possible.
  • the terms “general” and “generally” and “substantially” are intended to represent the inherent degree of uncertainty that is often attributed to any quantitative comparison, value, and measurement calculation, or other representation.

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Abstract

Un capteur de vent et un procédé de fabrication de direction de flux de vent et d'estimations et de prédictions de vitesse de flux de vent sont présentés. Le capteur de vent comporte un corps de coque sphérique, une multitude de prises de pression et une multitude de transducteurs de pression. Des optimisations de taille, de poids, de puissance et de coût (SWaP-C) peuvent être effectuées dans la conception et la construction du capteur de vent. Un modèle mathématique inverse et un apprentissage automatique sont utilisés dans la direction de flux de vent et des estimations de vitesse. Par rapport aux dispositifs antérieurs, le capteur de vent et le procédé présentent une fidélité améliorée.
PCT/US2023/030575 2022-08-18 2023-08-18 Capteur de vent et procédé de fabrication d'estimations de direction de vent et de vitesse de vent WO2024039845A1 (fr)

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090222150A1 (en) * 2005-09-27 2009-09-03 Airbus France System for monitoring anemobaroclinometric parameters for aircraft
US20110106324A1 (en) * 2009-09-28 2011-05-05 Sagie Tsadka Methods, devices and systems for remote wind sensing
US20200293594A1 (en) * 2016-06-02 2020-09-17 Brown University Physics informed learning machine

Patent Citations (3)

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Publication number Priority date Publication date Assignee Title
US20090222150A1 (en) * 2005-09-27 2009-09-03 Airbus France System for monitoring anemobaroclinometric parameters for aircraft
US20110106324A1 (en) * 2009-09-28 2011-05-05 Sagie Tsadka Methods, devices and systems for remote wind sensing
US20200293594A1 (en) * 2016-06-02 2020-09-17 Brown University Physics informed learning machine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
RICHARD M. ECKMAN, ET AL.: "A Pressure-Sphere Anemometer for Measuring Turbulence and Fluxes in Hurricanes", JOURNAL OF ATMOSPHERIC AND OCEANIC TECHNOLOGY, AMERICAN METEOROLOGICAL SOCIETY, BOSTON, MA, US, vol. 24, no. 6, 1 June 2007 (2007-06-01), US , pages 994 - 1007, XP055504486, ISSN: 0739-0572, DOI: 10.1175/JTECH2025.1 *

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