KR101894048B1 - System for managing aeronautical ground lighting - Google Patents

Abstract

The present invention relates to an aviation equalization management system, which measures the illuminance of an aviation equilibrium during moving of a moving object through an aviation equilibrium state measuring device, measures a speed state of a moving object during moving object movement through a moving object condition measuring device, Acquires distance data for aviation equalization based on the speed state of the moving object through the device and converts the illuminance state of the aviation equalization into the aviation equalization luminous intensity data using the obtained distance data for aviation equalization, By storing and managing the converted luminous intensity data of the aerial lighting according to the distance according to the distance, it is possible to quickly and accurately measure the luminous intensity state of the airborne lighting system while moving, and at the same time, As shown in FIG.

Description

SYSTEM FOR MANAGING AERONAUTICAL GROUND LIGHTING [0002]

FIELD OF THE INVENTION The present invention relates to aviation safety management systems, and more particularly, to aviation equalization management systems.

In general, an aircraft will use the aviation safety management system in all the processes of taking off and landing the airfield and landing on the airfield again. These aviation safety management systems can be collectively referred to as all facilities and systems that are installed to assist and support the navigation of aircraft by radio waves, lights, colors and shapes.

On the other hand, aviation safety management system can be classified into three types, namely, a navigation safety wireless facility using radio waves, an aviation equalization management system using lights, and an air traffic control facility exchanging information with voice.

Here, the aviation equilibrium management system is a system for managing aviation equilibrium. In order to securely operate the aviation equipments, the aviation equipments need to provide information, And maintenance of maintenance and repair work can be managed.

In particular, the conventional air-conditioning management system for maintaining and repairing air-conditioning lighting uses a method of visually checking air-conditioning lighting at the airfield or measuring the luminous intensity of air-conditioning lighting using a fixed luminous intensity measuring device.

However, there is a problem that the method of visually checking by an administrator can not accurately grasp the state of the light for the aviation equalization because individual differences may occur depending on the manager's career. In addition, the inspection method using the fixed luminous intensity measuring apparatus has a problem that the price of the fixed photometer is not only high but also heavy, it is difficult to move or handle, and in particular, the luminous intensity state of the air lighting is not immediately known. That is, there is a problem that the inspection method using the fixed luminous intensity measurement apparatus can not manage the luminous intensity state for the aviation equalization quickly and efficiently.

Accordingly, there is a need to develop an aviation equalization management system capable of efficiently and integrally managing the luminous intensity state by not only quick and accurate measurement of the luminous intensity state for the aviation equalization while moving, but also the aviation equalization.

Japanese Patent Laid-Open No. 1994-026890

SUMMARY OF THE INVENTION The present invention has been made in order to solve the above problems, and it is an object of the present invention to provide a method and apparatus for measuring light conditions for an aviation equipments in a fast and accurate manner, And the like.

In order to achieve the above-mentioned object, a first aspect of the present invention provides an air conditioner comprising: an aerial equalization state measuring device mounted on a moving object, the air conditioner state measuring device measuring an illuminance state of an airborne equalization provided in an airfield during moving of the moving object; A moving object state measuring device mounted on the moving object and measuring the velocity state of the moving object during the moving object; And a controller for receiving the velocity state of the moving object measured by the moving object condition measuring device and calculating the distance from the aviation equalization to the moving object on the basis of the velocity data to obtain distance data for aviation equalization, The light intensity data of the air-lighting system is converted into the light intensity data of the air-lighting system provided by the air-conditioning system, And an aviation equality management system that manages the aviation equality management system.

Here, the air-conditioner state measuring device measures the illuminance state of the air-conditioner at predetermined time intervals, and the moving-object-state measuring device measures the velocity state of the moving object at each specific time, Based on the velocity state of the moving object measured at a specific time provided from the moving object state measuring apparatus, distance data to the moving object located at the specific time zone on the basis of the aviation equalization to obtain distance data for aviation equalization, It is preferable to convert the illuminance state of the air-lighting system, which is measured by the air-conditioner state measuring apparatus, to the brightness data of the air-lighting system.

Preferably, the aviation equilibrium state measuring apparatus includes: a main body constituting an overall body;

And a plurality of illuminance sensors arranged on a side of the main body in a line and spaced apart from each other by a predetermined distance, wherein the illuminance status of the air-lighting is measured through the plurality of illuminance sensors, module; And a plurality of infrared sensors arranged in a line at a predetermined distance on either side of the main body, wherein each of the plurality of infrared sensors senses the airplane equalization and transmits the airplane equalization sensing state to the airplane equalization management device And a sensed state measurement module.

Preferably, the aviation equality management apparatus receives the aviation equalization sensing status transmitted from the sensing status measurement module, detects the aviation equalization, gives an identification number to the detected aviation equalization, Calculating a distance from the aviation equalization having the identification number to the moving object based on the speed state of the moving object provided from the moving object state measuring device on the basis of the detected time point of the aviation equalization, Acquires the distance data of the identification number of the air conditioner and obtains the illumination condition of the airplane equal to the identification number provided from the illumination condition measurement module by using the distance data for the airplane equalization to which the identification number is assigned, And converts the converted light intensity data into the light intensity data corresponding to the converted airway data The light intensity data for databasing can be stored and managed.

Preferably, when a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are horizontally arranged in a line spaced apart from each other at a predetermined interval on either side of the main body, The equalization management device calculates the horizontal angle using the distance data for the aerial equalization to which the identification number is assigned and the distance data to each illuminance sensor spaced at a predetermined interval based on the preset reference illuminance sensor, The brightness data for aviation equalization according to the distance by the identification number can be stored and managed in a database by the calculated horizontal angle.

Preferably, the aviation equality management apparatus can calculate the horizontal angle by the following expression (1).

(Equation 1)

Here, H is the horizontal angle, d is the distance from the aerial lighting with identification number to the reference illuminance sensor, and 1 is the distance from the reference illuminance sensor to each illuminance sensor.

Preferably, the reference illuminance sensor among the plurality of illuminance sensors and the reference infrared ray sensor among the plurality of infrared ray sensors are arranged on a straight line, and the airborne illuminator to which the identification number is assigned is detected by an infrared ray sensor other than the reference infrared ray sensor The air-quality equalization management apparatus may correct distance data from the reference infrared sensor to the detected infrared sensor in the distance data from the reference illuminance sensor to the respective illuminance sensors, The horizontal angle can be calculated by using the distance data for the aerial equalization to which the aerial image is given.

Preferably, the aviation equality management apparatus can calculate the horizontal angle by the following expression (2).

(Equation 2)

Where H is the horizontal angle, d is the distance from the aerial equalization to which the identification number is assigned, to the reference illuminance sensor, l is the distance from the reference illuminance sensor to each illuminance sensor, l ' It is the distance to the infrared sensor.

Preferably, when a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are vertically arranged in a line spaced apart from each other at a predetermined interval on either side of the main body, The equalization management device calculates the vertical angle using the distance data for the aerial equalization to which the identification number is assigned and the distance data to each illuminance sensor spaced at a predetermined interval based on the preset reference illuminance sensor, The brightness data for aviation equalization according to the distances of the identification numbers can be stored in a database and managed according to the calculated vertical angle.

Preferably, the aerial equalization state measuring device includes at least one ultrasonic sensor disposed on one side of the main body, measures a height from the ground to the ultrasonic sensor through the ultrasonic sensor, And a height condition measurement module for transmitting the height status of the apparatus to the air-conditioning management apparatus

Preferably, the aviation equality management apparatus receives the aviation equalization sensing status transmitted from the sensing status measurement module, detects the aviation equalization, gives an identification number to the detected aviation equalization, Calculating a distance from the aviation equalization having the identification number to the moving object based on the speed state of the moving object provided from the moving object state measuring device on the basis of the detected time point of the aviation equalization, Acquires the distance data of the identification number of the air conditioner and obtains the illumination condition of the airplane equal to the identification number provided from the illumination condition measurement module by using the distance data for the airplane equalization to which the identification number is assigned, And converts the converted light intensity data into the light intensity data corresponding to the converted airway data To the intensity data and the high state of the air equalization state measuring apparatus supplied from the high state measurement module for databasing it can be stored and managed.

Preferably, when a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are horizontally arranged in a line spaced apart from each other at a predetermined interval on either side of the main body, The equalization management device calculates the vertical angle based on the distance data for the aerial equalization to which the identification number is assigned and the height of the aerial equalization state measurement device provided from the height state measurement module, Can be stored and managed in the form of a database for each of the calculated vertical angles.

Preferably, the aviation equality management apparatus can calculate the vertical angle by the following expression (3).

(Equation 3)

Where V is the vertical angle, d is the distance from the aerial equalization to which the identification number is assigned, and h is the distance from the ground to the illuminance sensor.

Preferably, when a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are vertically arranged in a line spaced apart from each other at a predetermined interval on either side of the main body, The equalization management device calculates the horizontal angle using the distance data for the aviation equalization to which the identification number is assigned and the height of the air conditioner state measuring device provided from the height condition measurement module, Can be stored and managed in the form of a database for each of the calculated horizontal angles.

Preferably, the main body includes first to third regions each having a plurality of illuminance sensors and a plurality of infrared sensors, wherein the second region, which is the center region of the first region to the third region, The number of illuminance sensors and infrared sensors may be greater than three.

Preferably, each of the illuminance sensors provided in the first area and the third area is arranged in a line spaced apart from each other by a first distance, and each illuminance sensor provided in the second area is spaced apart from each other by a second distance, And the first spacing may be longer than the second spacing.

Preferably, each infrared sensor may be arranged in a line spaced at equal intervals.

Preferably, the illumination condition measurement module includes fifteen illumination sensors, and the sensing condition measurement module may include thirteen infrared sensors.

Preferably, the aviation equalization management device receives the aviation equalization detection status transmitted from the detection status measurement module, compares the aviation equalization detection status with a predetermined reference detection range, and determines that aviation equalization is detected when the comparison result is equal to or greater than the reference detection range have.

Preferably, the reference sensing range may range from 450 mV to 550 mV.

Preferably, the infrared sensor may have a viewing angle range of 1 degree to 25 degrees.

Preferably, the aviation equilibrium state measuring apparatus includes at least one color sensor disposed on one side of the main body, and the chromaticity state of the aviation equilibrium is measured through the color sensor and transmitted to the aviation equality management apparatus Wherein the aviation equality management module receives the aviation equilibrium chromaticity state transmitted from the chromaticity state measurement module and receives the aviation equilibrium brightness data corresponding to the aviation equilibrium distance based on the aviation equilibrium chromaticity state transmitted from the chromaticity state measurement module, And a chromaticity coordinate graph may be generated to control the operation of the display screen separately provided so as to be displayed.

Preferably, the aviation equalization state measuring apparatus includes at least one camera disposed on one side of the main body, and photographs a surrounding image including the aviation equalization through the camera, and transmits the captured image to the aviation equalization management apparatus The air conditioner management apparatus may further include at least one indicator line for indicating a moving direction of a moving object and surrounding images including aerial lighting transmitted from the image condition measurement module, The operation of the display screen provided separately may be controlled.

Preferably, the camera may include a CCD camera.

Preferably, the aviation equalization state measuring device includes at least one position sensor disposed on either side of the main body, and the positional state of the aviation equalization state measuring device is measured through the position sensor, The air conditioner management apparatus according to claim 1, further comprising a position state measurement module that transmits the position measurement state of the air conditioner state measurement device to the management device, The distance from the aviation equalization to the moving object may be calculated to obtain distance data for aviation equalization.

Preferably, the position sensor may include a DGPS (Differential Global Positioning System).

Preferably, the moving object state measuring apparatus may measure the velocity state of the moving object through at least one Doppler radar sensor (DRS).

Preferably, the aviation equality management device includes a data collection module for collecting the illuminance state of the airplane equal to the aviation equilibrium state measured by the aviation equalization state measuring device and the velocity state of the moving object measured by the moving object state measuring device; A power supply module for supplying electric energy to the air conditioner state measuring device and the moving object state measuring device; A display module for displaying luminosity data and a light distribution graph of aviation equalization according to the distances of the aerial lighting equipments on a display screen; And a control unit for controlling operation of the data acquisition module, the power supply module and the display module, receiving the speed state of the moving object from the data collection module, calculating the distance from the airplane equalization to the moving object, Acquires the distance data for the aviation equalization, converts the illuminance status of the aviation equalization provided from the data collection module to the aviation equalization brightness data using the obtained distance data for the aviation equalization, A control unit for controlling the operation of the display module so that the brightness data of the aviation equalization converted into the light distribution graph is displayed on the display screen, Modules.

Preferably, the aviation equality management apparatus may further include a controller for generating brightness condition information of the aviation equalization by analyzing brightness data of the aviation equalization according to the distances of the aviation equalization, It is possible to control the operation of the display screen separately provided so as to be stored and managed in a database.

Preferably, the luminous intensity status information of the aviation equalization includes at least one of the following: maximum luminous intensity information, minimum luminous intensity information, average luminous intensity information, luminous intensity information relative to the International Civil Aviation Organization (ICAO) standard, And brightness information.

Preferably, the aviation equality management apparatus compares the luminous intensity status information of the aviation equalization according to the distance by the aviation equalization with a predetermined reference value range, and determines whether there is an abnormality according to the comparison result, The operation of the display screen can be controlled.

According to the aviation equalization management system according to an embodiment of the present invention as described above, it is possible to measure the illuminance state of the aviation equalization during the movement of the moving object through the aviation equalization state measuring apparatus, And the distance data for the aviation equalization is acquired based on the speed state of the moving object through the aviation equilibrium management apparatus and the illuminance condition of the aviation equalization is calculated by using the obtained distance data for aviation equalization And converts the converted luminance data of the aerial lighting into a database in accordance with the distance according to the distance according to the aviation equilibrium, and stores and manages the luminous intensity data of the aviation equilibrium in accordance with the distance, thereby making it possible to quickly and accurately measure the luminous intensity state It is an efficient and integrated management of the luminous intensity status by each lighting There is a dot.

According to the present invention, it is possible to measure the illuminance state of the aviation equalization through the plurality of illuminance sensors, and detect the aviation equalization through the plurality of infrared sensors, respectively, It is possible to increase the accuracy of measurement speed and measurement data.

According to the present invention, a plurality of illuminance sensors and a plurality of infrared sensors are horizontally arranged and / or vertically arranged in a line spaced apart from each other at a predetermined interval on either side of the air- It is possible to measure the illuminance of a plurality of aviation equipments in accordance with whether a plurality of aviation equipments are detected while moving, and thus it is possible to increase the accuracy of measurement speed and measurement data.

In addition, according to the present invention, the brightness data for aviation equalization according to distances according to distance is stored in a database for each horizontal angle and / or vertical angle, and stored and managed through the aviation equalization management apparatus, thereby efficiently and integrally Not only can it be managed, but it also has the advantage of being able to grasp the luminous intensity state of each aerial lighting accurately.

Further, according to the present invention, by calculating the angle based on the corrected distance data on the luminance data for the aviation equalization along the distance through the aviation equality management apparatus, the angle can be precisely calculated, There is an advantage that it can grasp accurately.

In addition, according to the present invention, by calculating the angle based on the height condition of the aviation equalization state measuring apparatus measured in real time through the ultrasonic sensor, It is advantageous in that it can accurately grasp the luminous intensity of each lighting by angle.

In addition, according to the present invention, it is possible to measure the state of aviation equilibrium and moving objects by using various sensors such as an illuminance sensor, an infrared sensor, an ultrasonic sensor, a color sensor, a camera, a position sensor and a Doppler radar sensor (DRS) The accuracy can be improved.

According to the present invention, it is possible to improve the accuracy of the measurement data by comparing the aviation equalization detection state with the predetermined reference detection range through the aviation management device, and determining that the aviation equalization is detected when the comparison result is equal to or greater than the reference detection range There is an advantage.

According to the present invention, the brightness data of the aviation equalization is analyzed by the aviation equalization management device according to the distance of the aviation equalization to calculate the brightness state information of the aviation equalization (i.e., the maximum brightness information, the minimum brightness information, Information on brightness, brightness information on the basis of the International Civil Aviation Organization (ICAO) standard, vertical luminance information and horizontal luminance information), and stores the luminance state information of the generated aviation equalization in a database according to the distance according to the distance between the equipments, By displaying the light distribution graph and the chromaticity coordinate graph on the display screen, there is an advantage that the luminance state can be efficiently and integrally managed by the air lighting.

FIG. 1 is a block diagram of an entire aerial lighting management system according to an embodiment of the present invention. Referring to FIG.
FIG. 2A is an overall block diagram illustrating an aerial equalization state measuring apparatus according to an embodiment of the present invention.
FIG. 2B is a perspective view illustrating an apparatus for measuring an air-conditioner state applied to an embodiment of the present invention. FIG.
2C is a bottom view of an aerial equalization state measuring apparatus according to an embodiment of the present invention.
FIG. 2D is a conceptual diagram for explaining an aerial equalization state measuring apparatus applied to an embodiment of the present invention.
FIG. 3A is a block diagram illustrating a moving object condition measuring apparatus according to an embodiment of the present invention. Referring to FIG.
3B is a perspective view illustrating a moving object state measuring apparatus according to an embodiment of the present invention.
FIG. 3C is an exploded view of a moving object state measuring apparatus according to an embodiment of the present invention. FIG.
FIG. 4 is a block diagram of an entire aerial lighting management apparatus according to an embodiment of the present invention.
FIG. 5A is a conceptual diagram for explaining how an air-conditioning management system according to an embodiment of the present invention is disposed in a vehicle. FIG.
5B is a perspective view for explaining an aerial equalization state measuring apparatus and a moving object state measuring apparatus applied to an embodiment of the present invention mounted on a vehicle mount at the time of buried aerial equalization measurement.
FIG. 5C is a perspective view for explaining an aerial equalization state measuring apparatus and a moving object state measuring apparatus applied to an embodiment of the present invention mounted on a vehicle mount at the time of exposure-type airborne equalization measurement.
FIG. 5D is a side view illustrating a state where a moving object state measuring apparatus according to an embodiment of the present invention is mounted on an actual vehicle through a vehicle cradle. FIG.
FIG. 5E is a photograph showing a front view of a state where a moving object state measuring apparatus according to an embodiment of the present invention is mounted on an actual vehicle through a vehicle cradle. FIG.
6A is a conceptual diagram for explaining a horizontal angle calculation method applied to an embodiment of the present invention.
FIG. 6B is a diagram showing the horizontal angle calculated through FIG. 6A by distance.
6C is a conceptual diagram for explaining a method of correcting a horizontal angle applied to an embodiment of the present invention.
7A is a conceptual diagram for explaining a vertical angle calculation method applied to an embodiment of the present invention.
FIG. 7B is a diagram showing the vertical angles calculated through FIG. 7A by distance.
FIG. 8 is a diagram for explaining a method of converting a distance using a velocity state of a moving object measured through a Doppler radar sensor (DRS) applied to an embodiment of the present invention.
FIG. 9A is a view showing a viewing angle range of a front-facing infrared sensor for detecting airborne lighting in a vertical mounting measurement according to an embodiment of the present invention. FIG.
FIG. 9B is a diagram illustrating signal intensity of a front-facing infrared sensor applied to an embodiment of the present invention according to distance.
FIG. 10 is a view for explaining a method of generating a chromaticity coordinate graph using the chromaticity state of the aerial equalization measured through the color sensor applied to an embodiment of the present invention.
11A to 11C are views for explaining a buried aerial equalization measurement method applied to an embodiment of the present invention.
FIGS. 12A to 12C are views for explaining a method of measuring a temporal / terrestrial aerial equalization applied to an embodiment of the present invention.

BRIEF DESCRIPTION OF THE DRAWINGS The advantages and features of the present invention and the manner of achieving them will be more apparent from the following detailed description taken in conjunction with the accompanying drawings. The present invention may, however, be embodied in many different forms and should not be construed as being limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. Is provided to fully convey the scope of the invention to those skilled in the art, and the invention is only defined by the scope of the claims. Like reference numerals refer to like elements throughout the specification. "And / or" include each and every combination of one or more of the mentioned items.

Although the first, second, etc. are used to describe various elements, components and / or sections, it is needless to say that these elements, components and / or sections are not limited by these terms. These terms are only used to distinguish one element, element or section from another element, element or section. Therefore, it goes without saying that the first element, the first element or the first section mentioned below may be the second element, the second element or the second section within the technical spirit of the present invention.

The terminology used herein is for the purpose of illustrating embodiments and is not intended to be limiting of the present invention. In the present specification, the singular form includes plural forms unless otherwise specified in the specification. It is noted that the terms "comprises" and / or "comprising" used in the specification are intended to be inclusive in a manner similar to the components, steps, operations, and / Or additions.

Unless defined otherwise, all terms (including technical and scientific terms) used herein may be used in a sense commonly understood by one of ordinary skill in the art to which this invention belongs. Also, commonly used predefined terms are not ideally or excessively interpreted unless explicitly defined otherwise.

In the following description of the present invention, detailed description of known functions and configurations incorporated herein will be omitted when it may make the subject matter of the present invention rather unclear. The following terms are defined in consideration of the functions in the embodiments of the present invention, which may vary depending on the intention of the user, the intention or the custom of the operator. Therefore, the definition should be based on the contents throughout this specification.

Hereinafter, an airline equalization management system according to an embodiment of the present invention will be described with reference to the accompanying drawings.

FIG. 1 is a block diagram of an entire aerial lighting management system according to an embodiment of the present invention. Referring to FIG.

1, an aviation equalization management system according to an embodiment of the present invention includes an aviation equilibrium state measurement device 100, a moving object condition measurement device 200, an aviation equality management device 300, and the like .

Here, the aerial equalization state measuring apparatus 100 may be mounted on an object. In one example, the aerial equalization state measuring apparatus 100 may be mounted on a stationary object. In another example, the aerial equalization state measuring apparatus 100 may be mounted on a moving body. Here, the moving object is a moving object, and may include any object as long as it can move, but is not limited to, an automobile in general.

In another example, the aerial equalization state measuring device 100 may be mounted on a human body. Here, the term " mounted on a human body " may mean that the air-conditioning state measuring apparatus 100 has portability.

Also, the aviation equalization state measuring apparatus 100 can measure the illuminance state of the aviation equalization provided in the airfield during the movement of the moving object. That is, the aviation equalization state measuring apparatus 100 can measure the illuminance state of the aviation equalization at predetermined time intervals.

In one example, the aviation equilibrium state measurement device 100 can measure the illumination state of the airplane equalization in real time. In another example, the aviation equalization state measuring device 100 may periodically measure the illuminance status of the aviation equalization.

In another example, the aviation equalization state measuring apparatus 100 may measure the illuminance state of the airplane equalization at an arbitrary time (for example, when the illuminance state measurement signal is supplied from the airplane equalization management apparatus 300) .

Here, the aerial lighting provided in the aerodrome may be an equalization provided in a land area (for example, a building, a facility, and equipment) having the purpose of using all or a part of the aerodrome for the arrival, , Which may mean a security facility on the ground that helps to navigate the aircraft at normal, night, or bad weather.

For example, the aviation equalization may include at least one of flush and equalization equalization, but is not limited thereto and may include any equalization if it is an equalization that can help navigate the aircraft.

In addition, the aviation lighting can be classified into various types such as an aeronautical beacon, Approach Lighting Systems, Precision Approach Path Indicator, Circling Guidance Lights, Runway Edge Lights, Runway Threshold Identification Lights, Runway Center Line Lights, Runway Distance Marker Signature, Runway Threshold Lights, Runway Threshold Wing Bar Lights, Runway Threshold Identification Lights, Runway Center Line Lights, Runway end lights, taxiway edge lights, taxiway center line lights, runway guidance lights, etc., as well as emergency lighting, emergency lighting, Runway Guard Lights, Illuminated Wind Direction Indicator, Signaling Lamps, etc., as well as various other types of lamps, such as Runway Lead-in Lighting Systems, Intermediate Holding Position Lights, Stop Bar Lights, , Light Gun), landing room Landing Direction Indicator, Road-holding Position Lights, Stop Way Lights, Unserviceability Lights, Runway Turn Pad Lights, Aircraft Stand Identification Sign, Aircraft Stand Maneuvering Guidance Lights, Apron Floodlighting, Visual Docking Guidance System, Taxiway Guidance Sign, Deicing / (Deep / Anti-Icing Facility Exit Lights), Rapid Exit Taxiway Indicator lights, Heliport Beacon, Heliport Approach Lighting System, Aiming Point Lights, Landing Area, etc., are provided for the students to learn more about the program, such as Heliport Approach Path Indicator, Visual Alignment Guidance System, Final Approach & Take-off Area Lights, Area Lighting Syst em, winching area floodlighting, and floodlighting of obstacles, but may include any equalization, such as, but not limited to, an equalization that can help navigate the aircraft.

Here, the illuminance state of the air-lighting can be defined as energy (lm / m) received from a light source per unit area (e.g., aviation lighting) and expressed by unit lux (lx).

In addition, the aviation equalization state measuring apparatus 100 may transmit the measured illumination state of the aviation equalization to the aviation equalization managing apparatus 300 to be described later.

The mobile state measurement apparatus 200 can be mounted on an object. In one example, the mobile state measurement apparatus 200 may be mounted on a stationary object. In another example, the mobile state measurement apparatus 200 may be mounted on a mobile body. Here, the moving object is a moving object, and may include any object as long as it can move, but is not limited to, an automobile in general.

In another example, the mobile state measurement device 200 may be mounted on a human body. Here, the meaning of being mounted on the human body may mean that the mobile body condition measuring apparatus 200 has portability.

In addition, the moving object condition measuring apparatus 200 can measure the speed condition of the moving object while the moving object is moving. That is, the moving object state measuring apparatus 200 can measure the speed state of the moving object at predetermined time intervals.

In one example, the moving object condition measuring device 200 can measure the speed condition of the moving object in real time. In another example, the moving object condition measuring device 200 may periodically measure the speed condition of the moving object.

In another example, the moving object condition measuring apparatus 200 may measure the speed condition of the moving object at an arbitrary time (for example, when the speed condition measuring signal is received from the air-conditioning management apparatus 300).

In addition, the moving object condition measuring apparatus 200 may transmit the measured speed state of the moving object to the aviation equality management apparatus 300 to be described later.

Meanwhile, the aviation equalization state measuring apparatus 100 and the mobile body position measuring apparatus 200 may be integrated with each other as described above, but are not limited thereto and may be integrated into one component .

The aviation equalization management device 300 may be connected to the aviation equalization status measurement device 100. In addition, the aviation equalization management device 300 may receive the illuminance status of the measured aviation equalization from the aviation equalization status measurement device 100. [

In one example, the aviation equalization management device 300 can receive the illuminance status of the measured aviation equalization from the aviation equalization status measurement device 100 in real time. In another example, the aviation equalization management device 300 may be periodically provided with the illuminance status of the measured aviation equalization from the aviation equalization status measurement device 100. [

In another example, the aviation equalization management apparatus 300 may measure the illuminance state of the measured aviation equalization from the aviation equalization state measurement apparatus 100 at a certain time (for example, at a time when the illumination condition acquisition signal is received from the manager) Can be provided.

In addition, the aviation equality management apparatus 300 may be connected to the mobile state measurement apparatus 200. In addition, the aviation equality management apparatus 300 may receive the measured speed status of the moving object from the moving object condition measuring apparatus 200. [

In one example, the aviation equalization management device 300 can receive the measured velocity status of the moving object from the moving object condition measuring device 200 in real time. In another example, the aviation equalization management apparatus 300 may be periodically provided with the velocity state of the measured moving object from the moving body state measuring apparatus 200. [

In another example, the aviation equalization management apparatus 300 receives the velocity state of the measured moving object from the moving body condition measuring apparatus 200 at a certain time (for example, when the velocity state obtaining signal is received from the manager) .

In addition, the aviation equality management apparatus 300 may calculate the distance from the aviation equalization to the moving object based on the speed state of the moving object provided from the moving object condition measuring apparatus 200, have.

That is, the aviation equalization management device 300 calculates the distance to the moving object located at the specific time zone on the basis of the aviation equalization, based on the velocity state of the moving object measured for each specific time provided from the moving object state measuring device 200 And obtain the distance data for the aerial equalization.

For example, the aviation equality management apparatus 300 may include a lookup table storing a distance value corresponding to a speed value, a predetermined speed-distance relation and parameters (e.g., Time, slope, etc.), it is possible to calculate distance from the aviation equalization to the moving object to obtain distance data for aviation equalization. However, the present invention is not limited to this, and the speed state can be converted into distance data Any method and / or apparatus may be used.

The aviation equalization management device 300 may convert the illuminance state of the aviation equalization provided from the aviation equalization state measurement apparatus 100 into the aviation equalization luminous intensity data using the obtained distance data for aviation equalization.

That is, the aviation equalization management apparatus 300 uses the obtained distance data for aviation equalization to calculate the illuminance status of the aviation equalization measured for each specific time period, which is provided from the aviation equalization status measurement apparatus 100, . ≪ / RTI >

For example, the aviation equalization management device 300 may calculate distance information (e.g., distance by area, etc.) based on the obtained distance data for the aviation equalization and the illuminance status of the aviation equalization provided from the aviation equalization status measurement device 100 ) Using at least one of a look-up table stored with illuminance values and brightness values, predetermined illuminance-brightness relationships, and parameters (e.g., distance squared stars, etc.) to determine the illuminance status of the air- But it is not limited thereto, and any method and / or apparatus can be used as long as the illuminance state can be converted into luminous intensity data.

Here, the luminous intensity can be defined as the luminous energy (lm / sr) of light per unit solid angle, which is a bright degree of light (for example, light generated in aerial lighting) and expressed by a unit candela It is possible.

In particular, the candela (cd) is the square of the light source and the position (i.e., position ²⁾ the can be multiplied by calculation, and the illuminance (lux) and the square of the distance (i.e., meter ²⁾ a may be calculated by multiplying have. Such a candela (cd) can be used as a basic unit for representing energy of light according to the direction of a light source (for example, aviation lighting, etc.).

In addition, the aviation equality management apparatus 300 can store and manage the converted luminous intensity data of the air-like lighting according to the distance according to the aviation equalization, based on the luminous intensity data of the converted aviation equalization.

In addition, the aviation equality management apparatus 300 analyzes the brightness data of the aviation equalization according to the distance of the aviation equalization to generate the aviation equilibrium brightness state information, and calculates the brightness state information of the aviation equalization It is possible to control the operation of the display screen separately provided so as to be stored and managed in a database.

Here, the brightness state information of the aviation equilibrium includes at least one of the maximum brightness information for aviation equalization, the minimum brightness information, the average brightness information, the brightness information based on the International Civil Aviation Organization (ICAO) standard, the vertical brightness information, Information, but is not limited thereto, and may include any information as long as the information can be acquired from the luminance data of the aerial equalization.

In addition, the aviation equality management apparatus 300 compares the luminous intensity status information of the aviation equalization according to the distance by the aviation equalization with a preset reference value range, determines whether there is an abnormality according to the comparison result, It is possible to control the operation of the display screen.

For example, the aviation equality management apparatus 300 compares the luminous intensity status information of the aviation equalization according to the distance of the aviation equalization with a preset reference value range, determines that the comparison result is normal when the comparison result is equal to or greater than the reference value range, And controls the operation of the display screen so that the result of the determination can be displayed.

Here, the reference value range may be one value, but is not limited thereto and may be a plurality of values. The reference value range may be one, but is not limited thereto and may be plural. The reference value range may be a standard determined by the International Civil Aviation Organization (ICAO), but is not limited thereto and may be a standard set by an administrator and / or another organization.

As described above, the aviation equalization management system according to the embodiment of the present invention measures the illuminance state of the aviation equalization during the movement of the moving object through the aviation equalization state measuring apparatus, And obtains the distance data for the aviation equalization based on the speed state of the moving object through the aviation equilibrium management device and calculates the illuminance condition of the aviation equalization by using the obtained distance data for the aviation equalization, Data based on the converted aviation equilibrium is stored and managed in accordance with the distance according to the distance according to the aviation equilibrium. Thus, it is possible to quickly and accurately measure the luminous intensity state for the aviation equilibrium while moving, It is possible to efficiently and integrally manage the luminous intensity state by equalization.

Also, the aviation equalization management system according to an embodiment of the present invention analyzes the brightness data of the aviation equalization according to the distance according to the aviation equalization through the aviation equalization management device to calculate the brightness state information of the aviation equalization The luminance information, the luminance information, the minimum luminance information, the average luminance information, the luminance information against the International Civil Aviation Organization (ICAO) standard, the vertical luminance information and the horizontal luminance information), and generates the luminance state information of the generated air- And displays and displays the light distribution graph and the chromaticity coordinate graph on the display screen, thereby efficiently and integrally managing the light state by the air lighting.

2A to 2D are diagrams for explaining an aerial equalization state measuring apparatus applied to an embodiment of the present invention.

FIG. 2B is a perspective view illustrating an apparatus for measuring an air-conditioning state applied to an embodiment of the present invention. FIG. 2C is a perspective view of the air- FIG. 2D is a conceptual diagram for explaining an aerial equalization state measuring apparatus applied to an embodiment of the present invention. FIG.

2A to 2D, an aerial lighting state measuring apparatus 100 according to an embodiment of the present invention mainly includes a main body 110, an illuminance state measuring module 120, a sensing state measuring module 130, .

Here, the main body 110 may be formed as a whole body. That is, the main body 110 includes a lightness state measurement module 120, a sensed state measurement module 130, a height state measurement module 140, a chromaticity state measurement module 150, a video state measurement module 160, The status measurement module 170, and the like.

In addition, the body 110 may have a hexahedral shape (e.g., a rectangular parallelepiped) as shown in FIGS. 2B and 2C, but it is not limited thereto, and any shape .

The illuminance state measurement module 120 may include a plurality of illuminance sensors 122 arranged on one side of the main body 110 at regular intervals. In one example, the illumination condition measurement module 120 may include a plurality of illumination sensors 122 horizontally arranged in a line at a certain interval on either side of the main body 110. In another example, the illumination condition measurement module 120 may include a plurality of illumination sensors 122 vertically arranged in a line spaced apart from each other on either side of the main body 110.

The illuminance state measurement module 120 may measure the illuminance state of the air-condition lighting through the plurality of illuminance sensors 122 and transmit the measured illuminance state to the air-lighting uniformity management apparatus 300. In one example, the illuminance state measurement module 120 may measure the illuminance status of the air-condition lighting through the plurality of illuminance sensors 122 in real time, and transmit the measurements to the air-conditioner management apparatus 300.

In another example, the illuminance state measurement module 120 may periodically measure the illuminance status of the air-condition lighting through the plurality of illuminance sensors 122, respectively, and transmit the measurements to the air-conditioner management apparatus 300.

In another example, the illuminance state measurement module 120 may be configured to measure the illuminance (e.g., at a time when the illuminance status measurement signal is received from the air- And transmits the measurement result to the aviation equality management apparatus 300. [0050]

The illuminance measurement module 120 may include an illuminance sensor 122 for measuring the illuminance condition of the air-lighting, as described above, but it is not limited thereto, and if the illuminance condition of the air- Any sensor can be included.

The sensing state measurement module 130 may include a plurality of infrared sensors 132 arranged on a side of the main body 110 at regular intervals. In one example, the sensed state measurement module 130 may include a plurality of infrared sensors 132 horizontally arranged in a line spaced apart from one another on either side of the body 110. In another example, the sensed state measurement module 130 may include a plurality of infrared sensors 132 that are vertically arranged in a line and spaced apart from one another on either side of the body 110.

Here, the infrared sensor 132 may have a viewing angle range of 1 degree to 25 degrees (for example, a viewing angle range of 20 degrees), but the present invention is not limited thereto and the viewing angle range of the infrared sensor 132 may be modified .

The sensing state measurement module 130 may sense the air-conditioning lighting through the plurality of infrared-ray sensors 132 and transmit the air-conditioning lighting sensing state to the air-conditioning lighting management device 300. In one example, the sensing state measurement module 130 may sense the air-conditioning lighting through the plurality of infrared sensors 132 in real time and transmit the air-conditioning lighting sensing state to the air-conditioning lighting management device 300.

In another example, the sensing state measurement module 130 periodically senses the airplane equalization through a plurality of infrared sensors 132, respectively, and transmits the airplane equalization sensing state to the airplane equalization management device 300.

In another example, the sensed state measurement module 130 may be configured to determine whether the air conditioning (e.g., at the point of time when the sensing status measurement signal is received from the air conditioning management apparatus 300) And can transmit the aviation equalization detection state to the aviation equalization management apparatus 300. [

In addition, the sensing state measurement module 130 may include, but is not limited to, an infrared sensor 132 to sense airborne equalization, as described above, and may include any sensor capable of sensing airborne lighting have.

Meanwhile, the main body 110 may include first to third regions having a plurality of illuminance sensors 122 and a plurality of infrared sensors 132, respectively.

Here, the second area, which is the center area of the first area to the third area, may have a greater number of illuminance sensors 122 and infrared sensors 132 than the first area and the third area.

Each of the illuminance sensors 122 provided in the first area and the third area may be arranged in a line spaced apart from each other by a first distance, The first gap may be longer than the second gap, and the first gap may be longer than the second gap. In addition, each of the infrared sensors 132 may be arranged in a line spaced at equal intervals.

Here, the number of the light intensity sensors 122 may be 15, but the number of the light intensity sensors 122 is not limited thereto and may be modified by the administrator. The number of the infrared sensors 132 may be 13, but the number of the infrared sensors 132 may be modified.

As described above, the air-conditioning management system according to the embodiment of the present invention measures the illuminance state of the air-conditioning system through the plurality of illuminance sensors, detects the air-conditioning system through the plurality of infrared sensors, It is possible to measure the illuminance state for a plurality of aerial lighting according to whether a plurality of aerial lighting is detected, thereby improving the accuracy of the measurement speed and the measurement data.

2A to 2D, the aviation equality management apparatus 300 may be connected to the illumination condition measurement module 120. [ In addition, the aviation equality management apparatus 300 may be provided with the illuminance status of the aviation equalization from the illumination condition measurement module 120. In addition, the aviation equality management apparatus 300 may be connected to the sensed state measurement module 130. In addition, the aviation equalization management device 300 may be provided with the aviation equalization detection status from the detection status measurement module 130.

In addition, the aviation equality management apparatus 300 may detect the aviation equalization based on the aviation equalization detection status provided from the detection status measurement module 130, and may assign an identification number to the detected aviation equalization.

Here, the identification number may include any type of information as long as the identification information identifies the aviation equalization, i.e., information indicating only the aviation equalization to identify the aviation equalization, and can identify each of the detected aviation equalization.

For example, the aviation equalization management device 300 compares the aviation equalization detection status provided from the detection status measurement module 130 with a predetermined reference detection range, and if it is determined that aviation equalization is detected when the comparison result is equal to or greater than the reference detection range In addition, an identification number may be assigned to the detected air-to-air equalization.

Here, the reference sensing range may be a single value, but it is not limited thereto and may be a plurality of values. The reference sensing range may be one, but it is not limited thereto and may be plural.

In particular, the reference sensing range may have 500 mV, but is not limited thereto, and may have a range of 450 mV to 550 mV, and may be modified and implemented.

As described above, the aviation equalization management system according to the embodiment of the present invention compares the aviation equalization detection state with the predetermined reference detection range through the aviation management apparatus, and when the comparison result is equal to or greater than the reference detection range, It is possible to increase the accuracy of the measurement data.

In addition, the aviation equalization management device 300 may be configured to determine, based on the detected time point of the aviation equalization to which the identification number is assigned, based on the velocity state of the moving object provided from the moving object state measurement device 200, The distance to the moving object may be calculated to obtain the distance data for the aerial equalization to which the identification number is assigned.

Also, the aviation equalization management apparatus 300 may use the distance data for the aviation equalization to which the identification number is assigned, to determine the illuminance status of the aviation equalization provided with the identification number, which is provided from the illumination status measurement module 120, And converts the brightness data of the converted aerial image into a database in accordance with the distance according to the identification number, and stores and manages the brightness data for the aerial image.

As described above, the plurality of illuminance sensors 122 included in the illuminance state measurement module 120 and the plurality of infrared sensors 132 included in the sensed state measurement module 130 are installed in the body 110, They can be horizontally arranged in a line spaced apart from one side.

At this time, the aviation equalization management device 300 uses the distance data for the aviation equalization to which the identification number is assigned and the distance data to each illuminance sensor 122 spaced at a predetermined interval based on the preset reference illuminance sensor, The angle can be calculated.

Here, the reference illuminance sensor may be an illuminance sensor 122 disposed at the center of the main body 110, but it is not limited thereto. The reference illuminance sensor 122 may be disposed outside the center of the main body 110.

For example, the aviation equality management apparatus 300 can calculate the horizontal angle by the following equation (1).

(Equation 1)

Referring to Equation 1, H can be the calculated horizontal angle. And d may be the distance from the aerial lighting to which the identification number is assigned to the reference illuminance sensor (e.g., distance data for the aerial lighting provided with the identification number). And l may be the distance from the reference illuminance sensor to each illuminance sensor 122. [

The standard illuminance sensor and the plurality of infrared illuminance sensors 132 among the plurality of illuminance sensors 122 may be arranged in a straight line. In addition, the airline illuminated with the identification number may be infrared rays other than the reference infrared ray sensor Can be sensed by the sensor 132.

At this time, the aviation equalization management apparatus 300 corrects the distance data from the reference infrared sensor to the detected infrared sensor 132 in the distance data from the reference illuminance sensor to each illuminance sensor 122, The horizontal angle can be calculated using the data and the distance data for the aerial equalization to which the identification number is assigned.

For example, the aviation equality management apparatus 300 can calculate the horizontal angle by the following equation (2).

(Equation 2)

Referring to Equation 2, H can be the calculated horizontal angle. And d may be the distance from the aerial lighting to which the identification number is assigned to the reference illuminance sensor (e.g., distance data for the aerial lighting provided with the identification number). And l may be the distance from the reference illuminance sensor to each illuminance sensor 122. [ And, l 'may be the distance from the reference infrared sensor to the infrared sensor 132 detected.

Also, the aviation equality management apparatus 300 can store and manage luminous intensity data for aviation equalization according to the distance by the identification number in a database for each calculated horizontal angle, based on the calculated horizontal angle.

As described above, the plurality of illuminance sensors 122 included in the illuminance state measurement module 120 and the plurality of infrared sensors 132 included in the sensed state measurement module 130 are installed in the body 110, They may be vertically arranged in a line spaced apart from each other on one side.

At this time, the aviation equalization management device 300 uses the distance data for the aerial equalization to which the identification number is assigned and the distance data to each illuminance sensor 122 spaced at a predetermined interval on the basis of the preset reference illuminance sensor, The angle can be calculated.

In addition, the aviation equality management apparatus 300 can store and manage luminous intensity data for aviation equalization according to the distance according to the identification number, on the basis of the calculated vertical angle, based on the calculated vertical angle.

In addition, the aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention may further comprise a height condition measurement module 140. [

The height condition measurement module 140 may include at least one ultrasonic sensor 142 disposed on either side of the main body 110. The height state measurement module 140 measures the height of the corresponding air conditioner 100 from the ground through the ultrasonic sensor 142 to the air conditioner management apparatus 300).

In one example, the height condition measurement module 140 measures the height from the ground surface to the ultrasonic sensor 142 through the ultrasonic sensor 142 in real time, and determines the height of the air conditioner 100 To the aviation equalization management apparatus 300.

In another example, the height condition measurement module 140 periodically measures the height from the ground to the corresponding ultrasonic sensor 142 through the ultrasonic sensor 142, and determines the height of the corresponding air- To the aviation equalization management apparatus 300.

In another example, the altitude status measurement module 140 is configured to measure the altitude of the corresponding ultrasonic wave from the ground via the ultrasonic sensor 142 at a certain time (for example, when receiving the altitude status measurement signal from the aviation equality management apparatus 300) The height of the sensor 142 may be measured to transmit the height of the air conditioner 100 to the air conditioner management apparatus 300.

The height condition measurement module 140 may include an ultrasonic sensor 142 for measuring the height from the ground to the ultrasonic sensor 142 as described above. However, the present invention is not limited to this, Any sensor can be included as long as the height up to the sensor 142 can be measured.

2A to 2D, the aviation equality management apparatus 300 may be connected to the height condition measurement module 140. [ Also, the aviation equality management apparatus 300 may be provided with the height status of the aviation equilibrium state measurement apparatus 100 measured by the height condition measurement module 140.

In addition, the aviation equalization management device 300 may receive the aviation equalization detection status transmitted from the detection status measurement module 130, detect the aviation equalization, and may also provide an identification number to the detected aviation equalization.

In addition, the aviation equalization management device 300 may be configured to determine, based on the detected time point of the aviation equalization to which the identification number is assigned, based on the velocity state of the moving object provided from the moving object state measurement device 200, It is possible to obtain the distance data for the aerial equalization to which the identification number is assigned.

Also, the aviation equalization management apparatus 300 may use the distance data for the aviation equalization to which the identification number is assigned, to determine the illuminance status of the aviation equalization provided with the identification number, which is provided from the illumination status measurement module 120, The light intensity data for the converted air-lighting and the light intensity data for the corresponding air-illuminated state measuring device 100 provided from the height-state measurement module 140, ) Can be stored in a database and managed.

As described above, the plurality of illuminance sensors 122 included in the illuminance state measurement module 120 and the plurality of infrared sensors 132 included in the sensed state measurement module 130 are installed in the body 110, They can be horizontally arranged in a line spaced apart from one side.

At this time, the aviation equalization management device 300 uses the distance data for the aviation equalization to which the identification number is assigned and the height state of the aviation equalization state measurement device 100 provided from the height state measurement module 140, Can be calculated.

For example, the aviation equality management apparatus 300 can calculate the vertical angle by the following equation (3).

Referring to Equation 3, V may be the calculated vertical angle. And d may be the distance from the aerial lighting to which the identification number is assigned to the reference illuminance sensor (e.g., distance data for the aerial lighting provided with the identification number). And h may be the distance from the ground to the illuminance sensor 122 (e.g., the height of the air-conditioner state measuring apparatus 100, etc.).

In addition, the aviation equality management apparatus 300 can store and manage luminous intensity data for aviation equalization according to the distances for the identification numbers on the basis of the calculated vertical angles, based on the calculated vertical angles.

As described above, the plurality of illuminance sensors 122 included in the illuminance state measurement module 120 and the plurality of infrared sensors 132 included in the sensed state measurement module 130 are installed in the body 110, They may be vertically arranged in a line spaced apart from each other on one side.

At this time, the aviation equalization management device 300 uses the distance data for the aviation equalization to which the identification number is assigned and the height state of the aviation equalization state measuring apparatus 100 provided from the height state measurement module 140, Can be calculated.

In addition, the aviation equality management apparatus 300 can store and manage luminous intensity data for aviation equalization according to the distance by the identification number in a database by the calculated horizontal angle, based on the calculated horizontal angle.

As described above, in the air-conditioning management system according to the embodiment of the present invention, a plurality of illuminance sensors and a plurality of infrared sensors are horizontally arranged and arranged in a line at a predetermined interval on either side of the air- And / or vertically arranged, it is possible not only to measure all kinds of aerial lighting, but also to measure the illuminance condition for a plurality of aerial lighting according to whether a plurality of aerial lighting is detected while moving, Accuracy can be increased.

In addition, the aviation equality management system according to an embodiment of the present invention stores and manages luminous intensity data for aviation equalization according to distance by a horizontal angle and / or a vertical angle through the aviation equalization management device, It is possible to efficiently and integrally manage the luminous intensity state according to the equalization, and also to accurately grasp the luminous intensity state according to the aerial lighting.

Also, the aviation equalization management system according to an embodiment of the present invention calculates the angle based on the corrected distance data based on the distance data of the aviation equalization according to distance through the aviation equality management apparatus, It is possible to accurately grasp the luminous intensity state of each lighting according to the angle.

Also, in the air-conditioning management system according to an embodiment of the present invention, the brightness data for aviation equilibrium according to the distance is transmitted through the aviation equilibrium management apparatus to the height state of the aviation equilibrium state measurement apparatus measured in real time through the ultrasonic sensor It is possible to calculate the angle precisely, and it is possible to accurately grasp the luminous intensity state by the angle of flight according to the angle.

In addition, the aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention may further include the chromaticity state measuring module 150. [

The chromaticity state measurement module 150 may include at least one color sensor 152 disposed on either side of the body 110. The chromaticity state measurement module 150 may measure the chromaticity state of the aviation equalization through the color sensor 152 and transmit the measured chromaticity state to the aviation equalization management device 300.

In one example, the chromaticity state measurement module 150 may measure the chromaticity state of the aviation equalization through the color sensor 152 in real time and transmit it to the aviation equalization management device 300. In another example, the chromaticity state measurement module 150 may periodically measure the chromaticity state of the aviation equalization through the color sensor 152 and transmit it to the aviation equalization management device 300.

In another example, the chromaticity status measurement module 150 may determine the chromaticity of the aviation equalization through the color sensor 152 at a certain time (for example, when the chromaticity status measurement signal is received from the aviation equality management device 300) And transmits the measured state to the air-conditioning management apparatus 300. [

The chromaticity state measurement module 150 may also include a color sensor 152 for measuring the chromaticity state of the aviation equalization, as described above, but it is not limited thereto, and if the chromaticity state of the aviation equalization can be measured Any sensor can be included.

Meanwhile, the aviation equality management apparatus 300 may be connected to the chromaticity state measurement module 150. In addition, the aviation equality management apparatus 300 may be provided with the aviation equalization chromaticity state measured from the chromaticity status measurement module 150.

The aviation equality management apparatus 300 stores and manages the luminous intensity data of the aviation equalization according to the distance according to the aviation equilibrium according to the color, based on the aviation equalization chromaticity state provided from the chromaticity state measurement module 150 In addition, it is possible to control the operation of the display screen separately provided so as to generate a chromaticity coordinate graph.

In addition, the aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention may further include a video state measurement module 160. [

The video condition measurement module 160 may include at least one camera 162 disposed on either side of the body 110. In addition, the video condition measurement module 160 may capture a surrounding image including the aviation equalization through the camera 162 and transmit the captured image to the aviation equality management apparatus 300.

In one example, the video condition measurement module 160 may capture a surrounding image including aviation equalization through the camera 162 in real time and transmit the captured video to the aviation equalization management device 300. In another example, the video condition measurement module 160 periodically captures a surrounding image including the aviation equalization through the camera 162 and transmits the captured video to the aviation equality management apparatus 300.

In another example, the video condition measurement module 160 may be operable to determine, via the camera 162, at least one of a surrounding image including aviation equalization (e.g., at a point in time when the shooting signal is received from the aviation equalization management device 300) And transmits it to the aviation equality management apparatus 300. [0050]

In addition, the video condition measurement module 160 may include a camera 162 for capturing a surrounding image, including aviation equalization, as described above, but is not limited to capturing a surrounding video including aviation equalization If so, any sensor can be included.

In particular, the camera 162 may include a CCD camera, but may include any camera capable of capturing ambient images including, but not limited to, aerial lighting.

Meanwhile, the aviation equality management apparatus 300 may be connected to the video condition measurement module 160. In addition, the aviation equality management apparatus 300 may be provided with a surrounding image including aviation equalization photographed from the video condition measurement module 160.

In addition, the aviation equality management apparatus 300 may include a separate display unit (not shown) to display at least one leader line that can indicate the moving image of the moving object and surrounding images including the aviation equalization provided from the video condition measurement module 160, The operation of the screen can be controlled.

In addition, the aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention may further include the position state measurement module 170. [

The position state measurement module 170 may include at least one position sensor 172 disposed on either side of the body 110. The positional state measurement module 170 may measure the positional state of the aviation equalization state measuring device 100 via the position sensor 172 and transmit the measurement result to the aviation equalization managing device 300.

In one example, the positional status measurement module 170 may measure the positional state of the aviation equalization state measuring device 100 through the position sensor 172 in real time and transmit the measurement result to the aviation equalization managing device 300. In another example, the position-status measurement module 170 may periodically measure the positional state of the aviation equalization state measuring device 100 via the position sensor 172 and transmit the measurement result to the aviation equalization managing device 300. [

In another example, the position state measurement module 170 may be configured to measure the position of the corresponding air equalization state measuring device (e.g., a point at which the position state measurement signal is received from the air traffic light management apparatus 300) 100 to the aviation equality management apparatus 300. The aviation equality management apparatus 300 may be configured to measure the position of the air-

The positional status measurement module 170 may also include a position sensor 172 for measuring the positional state of the aviation equalization state measurement device 100, as described above, but is not limited to, Any sensor may be included as long as it can measure the positional state of the status measuring apparatus 100.

In particular, the position sensor 172 may include, but is not limited to, a GPS (Global Positioning System) and / or a DGPS (Differential Global Positioning System) If so, any device may be included.

Meanwhile, the aviation equality management apparatus 300 may be connected to the position state measurement module 170. In addition, the aviation equality management apparatus 300 may be provided with the positional state of the aviation equilibrium state measurement apparatus 100 measured from the position state measurement module 170.

In addition, the aviation equalization management apparatus 300 may use the position state of the aviation equalization state measuring apparatus 100 provided from the position state measurement module 170 and the velocity state of the moving object measured by the moving body state measuring apparatus 200 The distance from the aviation equalization to the moving object may be calculated to obtain distance data for aviation equalization.

Referring to FIG. 2B, the main body 110 of the aerial equalization state measuring apparatus 100 according to an embodiment of the present invention may be provided in a rectangular parallelepiped. On the upper surface of the main body 110, a position sensor 172, that is, a DGPS may be disposed at the center, and a carrying handle may be disposed on both sides of the center.

15 color sensors 122 may be disposed on the bottom of the main body 110. A color sensor 152 may be disposed at the center of the illuminance sensor 122, A camera 162, that is, a CCD camera may be disposed thereon. A cable connection portion may be disposed on the right side of the main body 110.

Referring to FIG. 2C, thirteen infrared sensors 132 may be disposed on the bottom surface of the main body 110, and an ultrasonic sensor 142 may be disposed on the left edge. A mounting portion (for example, a vehicle mount 400 or the like) may be disposed on a lower surface and a rear surface of the main body 110.

Referring to FIG. 2D, the main body 110 may be divided into a first region to a third region. Here, four illuminance sensors 122 and four infrared sensors 132 may be disposed in the first area and the third area, respectively. In particular, the four illuminance sensors 122 and the four infrared sensors 132 may be arranged in a line spaced at equal intervals.

In addition, seven illuminance sensors 122 and five infrared sensors 132 may be disposed in the second area. In particular, the spacing of the seven illuminance sensors 122 may be shorter than the interval of the five infrared sensors 132. That is, the illuminance sensor 122 may be arranged more densely than the infrared sensor 132.

An infrared sensor 132, a color sensor 152, a camera 162 (e.g., a CCD camera, etc.), and a position sensor 172 (for example, DGPS, etc.) can be placed.

As described above, the aviation equilization management system according to an embodiment of the present invention can be applied to various types of aviation equipments such as aviation, airborne, airborne, etc. by using various sensors such as an illuminance sensor, an infrared sensor, an ultrasonic sensor, a color sensor, a camera, a position sensor and a Doppler radar sensor By measuring the state of the equilibrium and the moving object, the accuracy of the measurement data can be improved.

3A to 3C are views for explaining a moving object condition measuring apparatus according to an embodiment of the present invention.

FIG. 3A is a block diagram illustrating a moving object state measuring apparatus according to an embodiment of the present invention. FIG. 3B is a perspective view of a moving object state measuring apparatus according to an embodiment of the present invention. FIG. 6 is an exploded view of a moving object condition measuring apparatus according to an embodiment of the present invention. FIG.

Referring to FIG. 3A, a moving object condition measuring apparatus 200 according to an embodiment of the present invention may include a main body 210, a speed measuring module 220, and the like.

Herein, the main body 210 may form an entire body. That is, the main body 210 supports or mounts the speed measurement module 220 or the like to be described later.

The speed measurement module 220 may measure the speed state of the moving object while the moving object is moving, and may transmit the measured speed state to the aviation equalization management device 300. That is, the speed measurement module 220 may measure the speed state of the moving object at predetermined time intervals, and transmit the measured speed state to the aviation equalization management device 300.

In one example, the speed measurement module 220 may measure the speed state of the moving object in real time and transmit it to the aviation equality management apparatus 300. In another example, the speed measurement module 220 may periodically measure the speed condition of the moving object and transmit it to the aviation equality management device 300.

In another example, the speed measurement module 220 may measure the speed state of the moving object at an arbitrary time (for example, when the speed state measurement signal is received from the air-conditioning management apparatus 300) 300).

In addition, the speed measurement module 220 may include at least one sensor of at least one weather radar sensor and a doppler radar sensor (DRS) 222, but is not limited to, Any sensor can be included if it can.

That is, the moving object state measuring apparatus 200 may measure at least one Doppler radar sensor through the DRS 222 to transmit the velocity state of the moving object to the aviation equalization management apparatus 300.

Referring to FIGS. 3B and 3C, the main body 210 of the moving body condition measuring apparatus 200 according to an embodiment of the present invention may have a hexahedron shape as shown in the figure, but is not limited thereto Any shape can be provided as long as it can support or mount a Doppler radar sensor (DRS) 222.

The body 110 may include a Doppler radar sensor (DRS) case, a Doppler radar sensor (DRS) case upper cover, a Doppler radar sensor (DRS) holder, and a microwave output unit.

FIG. 4 is a block diagram of an entire aerial lighting management apparatus according to an embodiment of the present invention.

4, an aviation equality management apparatus 300 according to an embodiment of the present invention includes a data acquisition module 310, a power supply module 320, a display module 330, a storage module 340, (350), and the like.

Here, the data acquisition module 310 may be connected to the control module 350. Also, the operation of the data acquisition module 310 can be controlled by the control module 350. That is, the data acquisition module 310 may collect data from the respective components under the control of the control module 350.

In one example, the data acquisition module 310 may collect data from each component in real time under the control of the control module 350. In another example, the data collection module 310 may periodically collect data from each component under the control of the control module 350. [

In another example, the data collecting module 310 collects data from each constituent element under the control of the control module 350 at a predetermined time (for example, a time when the data collection signal is received from the airplane equalization management apparatus 300) ). ≪ / RTI >

For example, the data acquisition module 310 may collect illumination conditions of the aerial lighting from the illumination condition measurement module 120. In addition, the data acquisition module 310 may collect the speed status of the mobile object from the mobile status measurement device 200 (e.g., the speed measurement module 220, etc.).

In addition, the data acquisition module 310 may collect the aviation equalization sensing status from the sensing status measurement module 130. In addition, the data acquisition module 310 may collect the height status of the aviation equalization state measuring apparatus 100 from the height state measurement module 140. The data acquisition module 310 may also collect the aviation equalization chromaticity status from the chromaticity status measurement module 150.

The data acquisition module 310 may also collect ambient images, including aviation equalization, from the video condition measurement module 160. The data acquisition module 310 may also collect the position status of the aviation equalization status measurement device 100 from the position status measurement module 170.

The power supply module 320 may be connected to the control module 350. In addition, the power supply module 320 can be controlled in operation by the control module 350. That is, the power supply module 320 can supply electric energy to the respective components under the control of the control module 350.

For example, the power supply module 320 may include components (e.g., a data acquisition module 310, a display module 330, a storage module 340, and a control module 350) provided in the air navigation management apparatus 300 ), And the like).

The power supply module 320 may also be connected to the aviation equalization status measuring device 100 (e.g., the illuminance status measurement module 120, the sensed status measurement module 130, the altitude status measurement module 140, (E.g., a motion state measurement module 150, a motion state measurement module 160, and a position state measurement module 170), and a mobile state measurement device 200 (e.g., a velocity measurement module 220).

The power supply module 320 may be an energy storage system (ESS). That is, the power supply module 320 may receive a DC power or an AC power from an external power supply. The power supply module 320 may charge electric energy corresponding to the supplied DC power or AC power. The power supply module 320 may supply the charged electric energy to the respective components described above.

For example, the power supply module 320 may include a power conversion unit, a battery charging unit, a battery, and a distribution unit.

Here, the power conversion unit may be connected to an external power source. Also, the power conversion unit may receive a DC power or an AC power from an external power source. In addition, the power conversion unit converts the supplied DC power or AC power to generate a converted power.

In one example, when the power source is a DC power source, the power conversion unit may include a DC-DC converter or a DC-AC converter. In another example, when the power source is an AC power source, the power conversion unit may include an AC-DC converter or an AC-AC converter.

The battery charging unit may be connected to the power conversion unit. In addition, the battery charging unit may receive power converted from the power converting unit. The battery charging unit may charge the battery with electrical energy corresponding to the converted power source.

The battery may be connected to a battery charging unit. In addition, the battery may be supplied with electric energy from the battery charging unit. In addition, the battery may be charged according to the electric energy supplied from the battery charging unit.

The distributor may be connected to a battery. In addition, the distributor may be provided with electric energy charged from the battery. Also, the distributing unit may distribute the charged electric energy to generate distributed electric energy having different sizes.

In addition, the distributing unit may provide the distributed electric energy to the respective components described above. Here, the distributing unit may include a Switching Mode Power Supply (SMPS) or the like.

The display module 330 may be coupled to the control module 350. In addition, the display module 330 can be controlled in operation by the control module 350. That is, the display module 330 may display data provided from each component (for example, the control module 350 or the like) on the display screen under the control of the control module 350.

For example, the display module 330 may be configured to display the illuminance of the aerial lighting, the speed state of the moving object, the distance data of the aerial lighting, the luminous intensity data of the aerial lighting, the luminous intensity data of the aerial lighting according to the distance by the aerial lighting, Brightness data for aviation equalization by vertical angle, brightness data for aviation equalization by vertical angle, brightness data for aviation equalization by vertical angle, aviation equalization chromaticity state, aviation equalization At least one indicator capable of indicating the moving direction of the moving object and the surrounding image, the positional state of the air-conditioner state measuring device 100, the luminance data and the light distribution graph of the air- At least one of the light condition of the air conditioner according to the distance of the air conditioner and the presence or absence of the light condition of the air conditioner is received from the control module 350 and displayed on the display screen But it not limited to this it is possible to display all of the data received from the respective component (For example, the control module 350, etc.) on the display screen.

The display module 330 may be a liquid crystal display (LCD), a light emitting diode (LED), a thin film transistor-liquid crystal display (TFT LCD), an organic light emitting diode Light Emitting Diode (OLED), Flexible Display, Plasma Display Panel (PDP), Surface Alternating Lighting (ALiS), Digital Light Source Processing (DLP), Silicon Liquid Crystal (LCoS) (TDEL), a quantum dot display (QD-SED), a field emission display (FED), a laser TV (quantum dots laser, a liquid crystal laser), a photodetector liquid display (FLD), an interferometer modulator display (iMoD) (LED), a telescopic pixel display (TPD), an organic light emitting transistor (OLET), a laser fluorescent display (LPD), or a 3D display But not limited to, any device capable of displaying the data provided from the control module 350. [0064]

The storage module 340 may be coupled to the control module 350. In addition, the storage module 340 can be controlled in operation by the control module 350. [ That is, the storage module 340 may store data provided from each component (for example, the control module 350, etc.) under the control of the control module 350.

For example, the storage module 340 may store the brightness data of the aerial lighting, the distance data of the aerial lighting, the brightness data of the aerial lighting, the brightness data of the aerial lighting according to the distance by the aerial lighting, Brightness data for aviation equalization by vertical angle, brightness data for aviation equalization by vertical angle, brightness data for aviation equalization by vertical angle, aviation equalization chromaticity state, aviation equalization At least one indicator capable of indicating the moving direction of the moving object and the surrounding image, the positional state of the air-conditioner state measuring device 100, the luminance data and the light distribution graph of the air- Information on the brightness of the air conditioner, and the presence or absence of the light condition of the air conditioner according to the distance of the air conditioner from the control module 350. However, Rather it may store all data received from the respective component (For example, the control module 350, and so on).

The storage module 340 may be a flash memory type, a hard disk type, a multimedia card micro type, a card type memory (e.g., SD or XD memory) (Random Access Memory), a static random access memory (SRAM), a read-only memory (ROM), an electrically erasable programmable read-only memory (EEPROM), a programmable read-only memory (PROM) A magnetic disk, and / or an optical disk.

On the other hand, the various embodiments described herein may be embodied in a recording medium readable by a computer or similar device using, for example, software, hardware, or a combination thereof.

According to a hardware implementation, the embodiments described herein may be applied to various types of devices such as Application Specific Integrated Circuits (ASICs), Digital Signal Processors (DSPs), Digital Dignal Processing Devices (DSPDs), Programmable Logic Devices (PLDs), Field Programmable Gate Arrays Processors, processors, microprocessors, microprocessors, microprocessors, microprocessors, and other electronic units for performing other functions. In some cases, the embodiments described herein may be implemented by the control module 350 itself.

According to a software implementation, embodiments such as the procedures and functions described herein may be implemented with separate software modules. Each of the software modules may perform one or more of the functions and operations described herein. Software code may be implemented in a software application written in a suitable programming language. The software code may be stored in a storage module 340, which will be described later, and may be executed by the control module 350. [

The control module 350 controls the components (for example, the data acquisition module 310, the display module 330, the storage module 340, and the power supply module 320) provided in the aviation equality management apparatus 300, Etc.), an aviation equalization state measurement device 100 (e.g., an illumination state measurement module 120, a sensing state measurement module 130, a height state measurement module 140, a chromaticity state measurement module 150, (E.g., module 160 and position state measurement module 170), and mobile state measurement device 200 (e.g., velocity measurement module 220, etc.).

For example, the control module 350 may receive the speed state of the moving object from the data collection module 310, and calculate the distance from the airplane equalization to the moving object on the basis of the speed state.

The control module 350 may convert the illuminance state of the air-lighting light received from the data collection module 310 into the light intensity data of the air-lighting system using the obtained distance data for the air-lighting.

The control module 350 then stores and manages the converted brightness data of the aviation equalization in accordance with the distance according to the aviation equilibrium based on the luminous intensity data of the aviation equalization, The operation of the display module 330 can be controlled so that the luminous intensity data of the aviation equilibrium is converted into the luminous intensity distribution graph and displayed on the display screen.

The control module 350 calculates the distance to the moving object located at the specific time zone based on the aviation equalization based on the velocity state of the moving object measured for each specific time provided from the data collection module 310, And obtains the distance data for the aviation equalization obtained from the data acquisition module 310 using the distance data for the aviation equalization to convert the illuminance condition of the aviation equalization measured for a specific time period into the luminous intensity data for aviation equalization have.

In addition, the control module 350 may receive the air-conditioning sensing state transmitted from the data acquisition module 310 to detect the air-conditioning lighting, and may provide an identification number to the detected air-conditioning lighting.

In the aviation equalization in which the identification number is assigned, based on the speed state of the moving object provided from the data collection module 310 on the basis of the detected time point of the aviation equalization to which the identification number is assigned, And obtains the distance data for the aerial equalization to which the identification number is assigned. The identification number provided from the data collection module 310 using the distance data for the aerial equalization Converts the illuminance state of the applied air-lighting into the luminous intensity data for the aviation equalization to which the identification number is assigned, and based on this, converts the luminous intensity data for the air-lighting equalized according to the distance by the identification number, .

In addition, the control module 350 may calculate the horizontal angle by using the distance data for the aerial equalization to which the identification number is assigned and the distance data to each illuminance sensor 122 spaced apart from each other by a predetermined reference illuminance sensor And based on this, brightness data for aerial equalization according to the distances of the identification numbers can be stored and managed in the form of a database for each calculated horizontal angle.

In addition, the control module 350 can calculate the horizontal angle by using the above-described equation (1).

In addition, the control module 350 may correct the distance data from the reference infrared sensor to the detected infrared sensor 132 in the distance data from the reference illuminance sensor to the respective illuminance sensors 122, The horizontal angle can be calculated using the distance data for the aerial equalization to which the identification number is assigned.

Further, the control module 350 can calculate the horizontal angle by using the above-described Equation (2).

In addition, the control module 350 may calculate the vertical angle using the distance data to the illuminance sensors 122, which are spaced apart from each other by a predetermined distance from the reference illuminance sensor, And based on this, brightness data for aviation equalization according to the distances of the identification numbers can be stored and managed in the form of a database for each of the calculated vertical angles.

In addition, the control module 350 receives the air-conditioning sensing state transmitted from the data acquisition module 310, detects the air-conditioning equalization, gives an identification number to the detected air-conditioning, The distance from the aviation equalization to which the identification number is assigned is calculated based on the speed state of the moving object provided from the data collection module 310 on the basis of the detected time point of the equalization, It is possible to obtain the distance data.

In addition, the control module 350 may use the distance data for the aviation equalization to which the identification number is assigned, to determine the illuminance status of the aviation equalization provided with the identification number, which is provided from the data collection module 310, The light intensity data for the converted air-lighting and the height state of the corresponding air-conditioning state measuring apparatus 100 provided from the data collection module 310, Can be stored in a database and managed.

The control module 350 calculates the vertical angle using the distance data for the aerial equalization to which the identification number is assigned and the height of the aerial equalization state measuring apparatus 100 provided from the data acquisition module 310, The brightness data for aviation equalization according to the distances of the identification numbers can be converted into a database for each of the calculated vertical angles.

In addition, the control module 350 can calculate the vertical angle using Equation 3 described above.

In addition, the control module 350 calculates the horizontal angle using the distance data for the aerial equalization to which the identification number is assigned and the height of the aerial equalization state measuring apparatus 100 provided from the data acquisition module 310, The brightness data for aviation equalization according to the distances of the identification numbers can be stored and managed in the form of a database for each of the calculated horizontal angles.

In addition, the control module 350 may compare the air-conditioning sensing condition transmitted from the data acquisition module 310 with a predetermined reference sensing range, and may determine that air-conditioning is detected when the comparison result is equal to or greater than the reference sensing range .

In addition, the control module 350 receives the aviation equalization chromaticity state transmitted from the data acquisition module 310, and based on the aviation equalization chromaticity status, It is possible to control the operation of the display screen separately provided so as to generate a chromaticity coordinate graph.

In addition, the control module 350 may include a separate display screen operation so that at least one leader line indicating the moving direction of the moving object and the surrounding image including the aerial equalization transmitted from the data collection module 310 may be displayed Can be controlled.

In addition, the control module 350 may also be configured to determine the position of the air conditioner from the aviation equalization using the positional state of the aviation equilibrium state measurement device 100 transmitted from the data acquisition module 310 and the velocity state of the moving object transmitted from the data acquisition module 310. [ The distance to the moving object can be calculated to obtain the distance data for the aerial equalization.

In addition, the control module 350 analyzes the brightness data of the aviation equalization according to the distance according to the aviation equalization to generate the luminous intensity state information of the aviation equalization, and calculates the luminous intensity state information of the aviation equalization, And can control the operation of the display screen separately provided so as to be displayed and stored.

In addition, the control module 350 compares the lightness state information of the air-like equalization according to the distance by the air-to-air equalization with a preset reference value range, determines whether there is an abnormality according to the comparison result, Can be controlled.

In addition, the control module 350 may control at least one of the illuminance state measurement signal, the velocity state measurement signal, the sensing state measurement signal, the height state measurement signal, the chromaticity state measurement signal, the photographing signal, the position state measurement signal, And transmits the generated signal to each corresponding component to control the operation of each component.

5A to 5E are views for explaining an air-like lighting management system according to an embodiment of the present invention disposed in a vehicle.

FIG. 5A is a conceptual diagram for explaining how an air-conditioning management system according to an embodiment of the present invention is disposed in a vehicle. FIG.

Referring to FIG. 5A, the air-conditioning management system according to an embodiment of the present invention may be disposed in a vehicle. Particularly, the data acquisition module 310, the power supply module 320, the display module 330, and the control module 350 of the aviation equality management apparatus 300 according to an embodiment of the present invention are independent of each other, As shown in FIG.

Also, the aviation equalization management system according to an embodiment of the present invention can mount the aviation equalization state measuring apparatus 100 and the moving object state measuring apparatus 200 on the vehicle using the vehicle mount 400. As shown in the figure, the vehicle mount 400 may be attached to the front surface of the vehicle so as to place the aerial equalization state measuring device 100 and the mobile state measuring device 200 on the front surface of the vehicle.

Here, the control module 350 applied to an exemplary embodiment of the present invention may be an administrator terminal. Such an administrator terminal may include a mobile communication terminal (for example, a smart phone) capable of transmitting and receiving data using wireless communication in real time or non-real time, but the present invention is not limited thereto. Any device capable of doing so can be included.

For example, the administrator terminal may be a personal computer (PC), a notebook computer, a personal digital assistant (PDA), a portable multimedia player (PMP), a PlayStation Portable (PSP) A server terminal such as a wireless communication terminal, a smart phone, a TV application server, and a service server, and may be a user terminal such as various devices or the like, or a communication modem such as a communication modem for performing communication with a wired or wireless communication network A microprocessor for executing and controlling a memory and / or program capable of storing programs and data for aviation equality management services, and the like.

5B is a perspective view for explaining an aerial equalization state measuring apparatus and a moving object state measuring apparatus applied to an embodiment of the present invention mounted on a vehicle mount at the time of buried aerial equalization measurement.

Referring to FIG. 5B, the aerial equalization state measuring apparatus 100 and the moving object state measuring apparatus 200, which are applied to an embodiment of the present invention, may be mounted on a vehicle mount 400.

Particularly, in the case of the buried aerial lighting measurement, the air conditioner state measuring apparatus 100 can be disposed in the approximate center portion of the vehicle mount 400, that is, in a substantially central portion of the vehicle, 400, that is, on the left and / or right portions with respect to the aerial equalization state measuring device 100. [

FIG. 5C is a perspective view for explaining an aerial equalization state measuring apparatus and a moving object state measuring apparatus applied to an embodiment of the present invention mounted on a vehicle mount at the time of exposure-type airborne equalization measurement.

Referring to FIG. 5C, the aerial equalization state measuring apparatus 100 and the moving object state measuring apparatus 200 according to an embodiment of the present invention may be mounted on a vehicle mount 400.

Particularly, in the exposure-type air-conditioning equalization measurement, the air-conditioner state measuring apparatus 100 can be disposed in the vehicle mount 400 outside the vehicle, and the mobile-state measuring apparatus 200 can be disposed at substantially both edges of the vehicle mount 400 , And may be disposed in the approximately left and / or right portion of the vehicle.

FIG. 5D is a side view illustrating a state in which a moving object state measuring apparatus according to an embodiment of the present invention is mounted on an actual vehicle through a vehicle cradle, FIG. 5E is a side view illustrating a moving object state measuring apparatus according to an embodiment of the present invention, Is a front view of a vehicle mounted on a vehicle through a cradle.

Referring to FIGS. 5D and 5E, the moving object condition measuring apparatus 200 according to an embodiment of the present invention can be disposed in the car cradle 400 as shown in the drawing, but is not limited thereto. And may be disposed on one side (for example, front, side, back, etc.).

In particular, the moving object state measuring apparatus 200 according to an embodiment of the present invention irradiates a plurality of beams onto the ground, receives a plurality of beams reflected from the ground, calculates a time difference between the signals, Can be measured.

6A to 6C are views for explaining a method of calculating a horizontal angle through an air-like lighting management system according to an embodiment of the present invention.

FIG. 6A is a conceptual diagram for explaining a horizontal angle calculation method applied to an embodiment of the present invention, FIG. 6B is a diagram illustrating horizontal angles calculated through FIG. 6A by distance, FIG. FIG. 7 is a conceptual diagram for explaining a method of correcting the applied horizontal angle.

Referring to FIG. 6A, a plurality of illuminance sensors 122-1 to 122-5 applied to an embodiment of the present invention may be horizontally arranged in a line spaced apart by a predetermined distance l. In particular, if the illuminance sensor disposed on a straight line with the aerial lighting (AGL) is referred to as a reference illuminance sensor 122-3, the illuminance sensors 122-1 and 122-2 , 122-4, 122-5). Here, the distance 1 from the reference illuminance sensor 122-3 to each of the illuminance sensors 122-1, 122-2, 122-4, and 122-5 may be information previously stored in the storage module 340 have.

Also, d may mean the distance from the aerial lighting (AGL) to the reference illuminance sensor 122-3. Here, the distance d from the aerial equalization (AGL) to the reference illuminance sensor 122-3 is calculated based on the distance data for aviation equalization calculated based on the velocity state of the moving object measured by the Doppler radar sensor (DRS) Lt; / RTI >

Therefore, the air-like lighting management system according to the embodiment of the present invention can control the distance from the reference illuminance sensor 122-3 to each illuminance sensor 122-1, 122-2, 122-4, And the distance d from the aerial lighting (AGL) to the reference illuminance sensor 122-3 into the above-described equation (1) to calculate the horizontal angle H.

Referring to FIG. 6B, FIG. 6B is a diagram illustrating the horizontal angle calculated by the above-described method according to distances, and the calculated horizontal angle H is wider as the moving object is located closer to the aviation equalization (AGL) .

6C, when the aviation equalization (AGL) is detected by the infrared sensor 132-5 (indicated by blue), the aviation equalization management system according to an embodiment of the present invention includes the reference illuminance sensor 122-3, (1) from the reference infrared sensor 132-4 to the respective illuminance sensors 122-1, 122-2, 122-4, and 122-5, the distance data 1 from the reference infrared sensor 132-4 to the infrared sensor 132-5 And the distance d from the aerial equalization (AGL) to the reference illuminance sensor 122-3 can be substituted into the equation (2) to calculate the corrected horizontal angle H.

Here, the distance data I 'from the reference infrared ray sensor 132-4 to the blue infrared ray sensor 132-5 may be information stored in advance in the storage module 340. [

FIGS. 7A and 7B are views for explaining a method of calculating a vertical angle through the air-conditioning management system according to an embodiment of the present invention.

FIG. 7A is a conceptual view for explaining a vertical angle calculation method applied to an embodiment of the present invention, and FIG. 7B is a diagram showing vertical angles calculated through FIG. 7A by distance.

7A, the aviation equalization management system according to the embodiment of the present invention calculates the distance d from the aviation equalization (AGL) to the reference illuminance sensor 122 and the distance d from the ground to the illuminance sensor 122 ) Can be substituted into the above-described formula (3) to calculate the vertical angle (V).

Here, the distance d from the aerial equalization (AGL) to the reference illuminance sensor 122 is the distance (d) to the aerial illumination (AGL) calculated based on the velocity state of the moving object measured by the Doppler radar sensor Lt; / RTI > The distance h from the ground to the illuminance sensor 122 may be the height of the air-conditioner state measuring apparatus 100 measured from the ultrasonic sensor 142.

Referring to FIG. 7B, FIG. 7B is a diagram showing vertical angles calculated by the above-described method by distance, and the calculated vertical angle V is larger as the moving object is located closer to the aviation equalization (AGL) .

FIG. 8 is a diagram for explaining a method of converting a distance using a velocity state of a moving object measured through a Doppler radar sensor (DRS) applied to an embodiment of the present invention.

Referring to FIG. 8, a Doppler frequency shift value applied to an embodiment of the present invention can be calculated through Equation 4 below.

(Equation 4)

는 Doppler shift[Hz]를 의미할 수 있다. 그리고,

는 Speed of light를 의미할 수 있다. 그리고,

는 Velocity를 의미할 수 있다. 그리고,

는 35.5 GHz(Ka band)를 의미할 수 있다. 그리고,

는 offset angle of sensor relative to direction of target motion을 의미할 수 있다.Referring to Equation 4,

Can mean Doppler shift [Hz]. And,

Can mean Speed of light. And,

Can mean Velocity. And,

May mean 35.5 GHz (Ka band). And,

May refer to an offset angle of sensor relative to a direction of target motion.

For example, when the output of the Doppler radar sensor DRS is 2600 Hz and the installation angle is 30 degrees, the actual velocity may be [2600 Hz / (100 Hz / mph)] / cos 30 ° = 30.02 mph. If the output of the Doppler radar sensor DRS is 2600 Hz and the installation angle is 31 degrees, the actual velocity may be 2600 Hz / (100 Hz / mph) / cos 31 degrees = 30.33 mph.

Accordingly, the output of the Doppler radar sensor (DRS) 222 applied to an embodiment of the present invention is converted into a distance as follows.

For example, when the output frequency is 100 Hz, since the velocity is 1 mph, the distance of 1 pulse is 1/60 (time) / 60 (minute) / 100 (pulse number per second) = 2.77778e-6 mi and 2.77778e -6 [mi] = 0.0146666784 [ft] = 4.4704 [mm], the distance per pulse can be calculated as 4.4704 mm.

When the distance is calculated using the total amount of pulses output from the Doppler radar sensor DRS (for example, the accumulated total number of pulses is 5,000,000 pulses, etc.), the distance is 5,000,000 x 2.77778e-6 [mi] 13.8889 [mi] = 22.352 [km].

Further, when the offset angle is applied to the calculated distance, the distance can be calculated as 5,000,000 x 2.77778e-6 [mi] x cos 30 ° = 12.02814 [mi] = 19.357494 [km].

9A and 9B are views for explaining a front-facing infrared sensor applied to an embodiment of the present invention.

FIG. 9A is a view showing a viewing angle range of a front-facing infrared ray sensor for detecting airborne lighting in a vertical mounting measurement according to an embodiment of the present invention, FIG. 9B is a front- FIG.

Hereinafter, the front detecting infrared ray sensor will be referred to as an infrared ray sensor 132. FIG.

The infrared sensor 132 disposed on the lower surface of the main body 110 of the aerial equalization state measuring apparatus 100 according to an embodiment of the present invention has a viewing angle range of 1 degree to 25 degrees (for example, a viewing angle range of 20 degrees) And is superimposed on a sensor-by-sensor basis, so that the aviation equalization state measuring apparatus 100 can detect the aviation equalization (AGL) even if it passes the aviation equalization (AGL).

Referring to FIG. 9A, in the vertically aligned aerial equalization measurement method applied to an embodiment of the present invention, the infrared sensor 132 applied to an embodiment of the present invention moves horizontally at 5 m ahead of the aerial lighting (AGL) If the viewing angle is designed to be 1 degree as shown in the drawing, the aviation equalization management system according to the embodiment of the present invention can accurately detect the aerial lighting (AGL) installed horizontally .

Referring to FIG. 9B, the infrared sensor 132 applied to the embodiment of the present invention outputs a signal less than a reference sensing range (for example, 500 mV or the like) at a normal time. However, , 500 mV, etc.) can be output. In addition, when one infrared sensor 132 of the 13 infrared sensors 132 applied to the embodiment of the present invention outputs a signal of a reference sensing range (for example, 500 mV or the like) The aviation equalization management device 300 can determine that the aviation equalization (AGL) is detected and can perform the aviation equalization count.

In addition, the air-conditioning management system according to an embodiment of the present invention can set the horizontal axis of the infrared sensor 132 that outputs the highest signal among the infrared sensors 132 to 0, and the infrared sensor 132 ) Can be set as a vertical axis.

FIG. 10 is a view for explaining a method of generating a chromaticity coordinate graph using the chromaticity state of the aerial equalization measured through the color sensor applied to an embodiment of the present invention.

Referring to FIG. 10, the three sensors X, Y, and Z applied to one embodiment of the present invention may have a common cathode line bundled with a cathode. Therefore, the aviation equalization management system according to an embodiment of the present invention constructs a trans-impedance measurement circuit using an OP-amp to measure the current of the color sensor 152, which changes according to the color of incident light, Can be calculated.

In the aviation equalization management system according to an embodiment of the present invention, the color sensor 152 measures signals for standard color samples and calculates final color coordinates X, Y, and Z according to the following procedure, Can be converted into a color coordinate using the three color signals coming from the color converter 152.

① Measure target data T and sensor data S

T = X1, Y1, Z1, ..., Xn, Yn, Zn

S = XADC1, YADC1, ZADC1, ..., XADCn, YADCn, ZADCn

② Measure the background signals

B = Xd, Yd, Zd

③ Correct the sensor signals

S '= S - B (ex: X' = Xadc - Xd)

④ Normalize the color data

- 4-1 find min, and max both in T and S 'data

T = Xmin, Ymin, Zmin < == > Xmax, Ymax, Zmax

S '= Xadcmin, Yadcmin, Zadcmin <==> Xadcmax, Yadcmax, Zadcmax

- 4-2 Calculate RGB offset

Roffset = Xadcmin - {(Xadcmax - Xadcmin) / (Xmax - Xmin)} xXmin

Goffset = Yadcmin - {(Yadcmax - Yadcmin) / (Ymax - Ymin)} x Ymin

Boffset = Zadcmin - {(Zadcmax - Zadcmin) / (Zmax - Zmin)} x Zmin

⑤ Adjust sensor data with RGB offset

S "= S '- (Roffset, Goffset, Boffset)

(ex: X '' = X'adc - Roffset)

⑥ Calculate color coeffitient

K = (T x S "trans) (S" x S "trans) -1

⑦ Calculate color coordinates

X, Y, Z = K x S "

● Target: Standard color plate with known color coordinates X, Y, Z

● Sensor: Sensor ADC output value which measured standard plate using mazet sensor

11A to 11C are views for explaining a buried aerial equalization measurement method applied to an embodiment of the present invention.

Referring to FIG. 11A, an aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention may be mounted on a vehicle mount 400 and disposed 180 mm from the ground. That is, the aviation equalization state measuring apparatus 100 may have a height of 180 mm.

The plurality of illuminance sensors 122 and the plurality of infrared sensors 132 provided in the air conditioner status measuring apparatus 100 according to an embodiment of the present invention are spaced apart from each other at a predetermined interval And can be horizontally arranged in a line.

In addition, since the vertical angle applied to the embodiment of the present invention can be changed according to the height of 180 mm, the air-like lighting management system according to the embodiment of the present invention is capable of real- The height of the measuring device 100 is measured and the height of the measured air-conditioner 100 is compared with the height of 180 mm. If the height of the comparison result is changed, that is, If the height of the measurement apparatus 100 does not match the height of 180 mm, the vertical angle can be calculated by correcting the height according to the height of the measured air-conditioner 100.

Referring to FIG. 11B, the aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention may be installed in front of a vehicle to measure a measurement area.

Referring to FIG. 11C, data measured through the aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention is converted into angle-specific data through the aerial equalization management apparatus 300 as shown in the figure And can be generated by the light distribution data.

That is, the aviation equalization management apparatus 300 applied to an embodiment of the present invention may be configured to provide the brightness of the aviation equalization through the arrangement of the illuminance sensor 122 and the distance data for aviation equalization based on the Doppler radar sensor (DRS) The data can be converted into angle-dependent data and converted into the light distribution data. In addition, the aviation equality management apparatus 300 applied to the embodiment of the present invention can calculate and output each measurement data according to the ICAO standard using the converted light distribution data.

Here, the distance data for the aerial equalization based on the Doppler radar sensor (DRS) 222 may be a vertical angle, and the arrangement of the illuminance sensors 122 for each distance may be a horizontal angle.

FIGS. 12A to 12C are views for explaining a method of measuring a temporal / terrestrial aerial equalization applied to an embodiment of the present invention.

Referring to FIG. 12A, the aerial lighting of the aerodrome can be installed laterally. Meanwhile, the buried aerial equalization measurement method described above with reference to FIGS. 11A to 11C is a method of measuring aerial equalization installed as a bipedal. Since the aerial equalization measurement is performed one by one in the horizontal aerial equalization measurement, time can be increased.

Accordingly, the aerial aerial illumination measurement method applied to the embodiment of the present invention can quickly measure the aerial illumination installed laterally through the vertical array scanning method. Here, the vertical array scanning method may be a method of vertically mounting the air conditioner 100 on the vehicle and measuring the state of the air conditioner.

Meanwhile, as shown in the figure, the illuminance equalization sensor 122 or the infrared sensor 132 may have a height of 100 mm, as shown in the figure.

That is, a plurality of illuminance sensors 122 and a plurality of infrared sensors 132 provided in the air-conditioning state measuring apparatus 100 according to an embodiment of the present invention are spaced apart from each other at a predetermined interval And can be vertically arranged in a line.

Referring to FIG. 12B, the aerial equalization state measuring apparatus 100 according to an embodiment of the present invention is capable of measuring a horizontal plane at a certain distance while moving transversely in front of an aerial equalization 5 m.

Referring to FIG. 12C, data measured through the aerial equalization state measuring apparatus 100 applied to an embodiment of the present invention is converted into angle-specific data through the aerial equalization management apparatus 300 as shown in the figure And can be generated by the light distribution data.

Here, the vertically arranged illuminance sensor 122 may be a vertical angle, and the moving distance, i.e., distance data for aviation equalization may be a horizontal angle.

Although the preferred embodiments of the air-conditioning management system according to the present invention have been described above, the present invention is not limited thereto, and various modifications may be made within the scope of the claims, And this also belongs to the present invention.

100: aerial equalization state measuring device 110: main body of aerial equalization state measuring device
120: illuminance state measurement module 122: illuminance sensor
130: sensing state measurement module 132: infrared sensor
140: height state measurement module 142: ultrasonic sensor
150: chromaticity state measurement module 152: color sensor
160: video condition measurement module 162: camera
170: Position state measurement module 172: Position sensor
200: Moving object state measuring device 210: Main body of moving object state measuring device
220: speed measuring device 222: Doppler radar sensor (DRS)
300: aviation equalization management device 310: data acquisition module
320: power supply module 330: display module
340: storage module 350: control module
400: Car Cradle

Claims (31)

An aerial equalization state measuring device mounted on a moving object and measuring an illuminance state of an aerial image provided in an aerodrome during the moving of the moving object;
A moving object state measuring device mounted on the moving object and measuring the velocity state of the moving object during the moving object; And
The distance measurement unit obtains distance data for aviation equalization by calculating the distance from the aviation equalization to the moving object on the basis of the velocity state of the moving object measured by the moving object condition measuring apparatus, And converts the illuminance status of the aviation equalization received from the aviation equilibrium state measurement device into luminous intensity data of the aviation equalization. Based on this, the luminous intensity data of the converted aviation equalization is stored in the database according to the distance according to the aviation equalization, The air-conditioning management apparatus comprising:
The air conditioner status measuring apparatus includes a main body constituting an overall body and a plurality of illuminance sensors arranged in a line spaced apart from each other by a predetermined distance on either side of the main body, And a plurality of infrared sensors arranged in a line and spaced apart from each other by a predetermined distance on one side of the main body, wherein the plurality of infrared sensors are connected to the air- And a sensing state measurement module for sensing the air-conditioner sensing state and transmitting the air-conditioning sensing state to the air-conditioning management apparatus.
The method according to claim 1,
Wherein the air-conditioner state measuring device measures the illuminance state of the air-conditioning lighting at predetermined time intervals, and the moving object state measuring device measures the velocity state of the moving object at each specific time, The distance to the moving object located at the specific time zone is calculated on the basis of the aviation equilibrium based on the velocity state of the moving object measured at a specific time provided from the measuring device to obtain distance data for aviation equilibrium, And converts the illuminance state of the air-lighting system, which is measured from the air-conditioning state measuring apparatus, to the lightness data for the air-lighting system, the distance data being used for the equalization.
delete The method according to claim 1,
The air-conditioning management apparatus includes an air-conditioning control unit that receives the air-conditioning sensing state transmitted from the sensing state measurement module, detects the air-conditioning, identifies the detected air-conditioning unit, The distance from the aviation equalization to which the identification number is assigned is calculated based on the velocity state of the moving object provided from the moving object state measuring apparatus on the basis of the detected point, Acquires the illuminance condition of the air-lighting equalized with the identification number provided from the illuminance-status measurement module using the distance data for the air-lighting equalization to which the identification number is assigned, Data based on the distance, and based on the distance, Air equalization management system which comprises the data storage and databasing management.
5. The method of claim 4,
When a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are horizontally arranged in a line spaced apart from each other at a predetermined distance on either side of the main body,
The aviation equality management apparatus calculates the horizontal angle using the distance data for the aviation equalization to which the identification number is assigned and the distance data to each illuminance sensor spaced a predetermined distance from the predetermined reference illuminance sensor, And the brightness data for aviation equalization according to the distance by the identification number is stored in a database for each calculated horizontal angle, and is stored and managed.
6. The method of claim 5,
Wherein the aviation equality management apparatus calculates a horizontal angle by the following Equation (1).
(Equation 1)

Here, H is the horizontal angle, d is the distance from the aerial lighting with identification number to the reference illuminance sensor, and 1 is the distance from the reference illuminance sensor to each illuminance sensor.
6. The method of claim 5,
When the reference illuminance sensor among the plurality of illuminance sensors and the reference infrared ray sensor among the plurality of infrared ray sensors are arranged on a straight line and the air equalization imparted with the identification number is detected by an infrared ray sensor other than the reference infrared ray sensor,
Wherein the air-quality equalization management device corrects distance data from the reference infrared sensor to the sensed infrared sensor on the basis of distance data from the reference illuminance sensor to each illuminance sensor, Wherein the horizontal angle is calculated using the distance data for the aerial equalization.
8. The method of claim 7,
Wherein the aviation equality management apparatus calculates a horizontal angle by the following expression (2).
(Equation 2)

Where H is the horizontal angle, d is the distance from the aerial equalization to which the identification number is assigned, to the reference illuminance sensor, l is the distance from the reference illuminance sensor to each illuminance sensor, l ' It is the distance to the infrared sensor.
5. The method of claim 4,
When a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are vertically arranged in a line spaced apart from each other at a predetermined distance on either side of the main body,
The aviation equality management apparatus calculates the vertical angle using the distance data for the aerial lighting with the identification number and the distance data to each illuminance sensor spaced at a predetermined interval based on the preset reference illuminance sensor, And stores the luminous intensity data for aviation equalization according to the distance according to the identification number into a database for each calculated vertical angle, and stores and manages the luminous intensity data.
The method according to claim 1,
The air-conditioning state measuring apparatus includes:
The height of the air conditioner is measured by the ultrasonic sensor through the ultrasonic sensor to measure the height from the ground to the ultrasonic sensor, And a height state measurement module for transmitting the altitude information.
11. The method of claim 10,
The air-conditioning management apparatus includes an air-conditioning control unit that receives the air-conditioning sensing state transmitted from the sensing state measurement module, detects the air-conditioning, identifies the detected air-conditioning unit, The distance from the aviation equalization to which the identification number is assigned is calculated based on the velocity state of the moving object provided from the moving object state measuring apparatus on the basis of the detected point, Acquires the illuminance condition of the air-lighting equalized with the identification number provided from the illuminance-status measurement module using the distance data for the air-lighting equalization to which the identification number is assigned, Data based on the distance, and based on the distance, Data and equalizing air control system, characterized in that to store and manage a database of high states of the air equalization state measuring apparatus supplied from the high state measurement module.
12. The method of claim 11,
When a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are horizontally arranged in a line spaced apart from each other at a predetermined distance on either side of the main body,
The aviation equality management apparatus calculates a vertical angle based on the distance data for the aviation equalization to which the identification number is assigned and the height of the aviation equality state measuring apparatus provided from the height state measurement module, And stores the luminous intensity data for the aviation equalization according to the star distance into a database for each of the calculated vertical angles, and stores and manages the luminous intensity data.
13. The method of claim 12,
Wherein the aviation equality management apparatus calculates a vertical angle by the following expression (3).
(Equation 3)

Where V is the vertical angle, d is the distance from the aerial equalization to which the identification number is assigned, and h is the distance from the ground to the illuminance sensor.
12. The method of claim 11,
When a plurality of illuminance sensors provided in the illuminance state measurement module and a plurality of infrared sensors provided in the sensed state measurement module are vertically arranged in a line spaced apart from each other at a predetermined distance on either side of the main body,
The aviation equality management apparatus calculates a horizontal angle based on the distance data for the aviation equalization to which the identification number is assigned and the height of the aviation equality state measuring apparatus provided from the height state measurement module, Wherein the brightness data for aviation equalization according to the star distance is stored in a database and managed according to the calculated horizontal angle.
The method according to claim 1,
The main body includes first to third regions each having a plurality of illuminance sensors and a plurality of infrared sensors,
Wherein a plurality of illuminance sensors and infrared sensors are provided in a second area, which is a center area of the first area to the third area, than the first area and the third area.
16. The method of claim 15,
Wherein each of the illuminance sensors provided in the first area and the third area is arranged in a line spaced apart from each other by a first distance and each illuminance sensor provided in the second area is arranged in a line spaced apart by a second distance, Wherein the first interval is longer than the second interval.
16. The method of claim 15,
Wherein each of the infrared sensors is arranged in a line spaced apart at equal intervals.
The method according to claim 1,
Wherein the illumination condition measurement module includes fifteen illuminance sensors, and the sensing state measurement module includes thirteen infrared sensors.
The method according to claim 1,
Wherein the aviation equalization management device receives the aviation equalization detection status transmitted from the detection status measurement module and compares the aviation equalization detection status with a predetermined reference detection range and determines that aviation equalization is detected when the comparison result is equal to or greater than the reference detection range Aviation Equalization Management System.
20. The method of claim 19,
Wherein the reference sensing range has a range of 450 mV to 550 mV.
The method according to claim 1,
Wherein the infrared sensor has a viewing angle range of 1 to 25 degrees.
The method according to claim 1,
The air conditioner status measuring apparatus includes at least one color sensor disposed on one side of the main body, the chroma status of the air conditioner is measured through the color sensor and transmitted to the air conditioner management apparatus Further comprising a measurement module,
The aviation equality management apparatus receives the aviation equilibrium chromaticity state transmitted from the chromaticity state measurement module, and based on the received aviation equilibrium chromaticity state, the aviation equality management apparatus stores and manages the luminous intensity data of the aviation equalization according to the distance by the aviation equalization, Wherein the control unit controls the operation of the display screen separately provided so as to generate a graph and display it.
The method according to claim 1,
The air conditioner status measuring apparatus may include at least one camera disposed on one side of the main body, and may further include a camera for capturing a surrounding image including aviation equalization through the camera, Further comprising a measurement module,
The aviation equality management apparatus may control the operation of a separate display screen so that at least one leader line capable of indicating a moving direction of a moving object and a surrounding image including aviation equalization transmitted from the video condition measurement module may be displayed, The air-conditioning management system comprising:
24. The method of claim 23,
Wherein the camera comprises a CCD camera.
The method according to claim 1,
The air conditioner status measuring apparatus includes at least one position sensor disposed on one side of the main body and measures the positional state of the corresponding air conditioner state measuring device through the position sensor, Further comprising a position state measurement module for transmitting the position state measurement module,
The air-like equilibrium management device may calculate a distance from the aviation equalization to the moving object by using the positional state of the aviation equalization state measuring device transmitted from the position state measurement module and the velocity state of the moving object measured by the moving object state measuring device And obtains the distance data for the aviation equalization.
26. The method of claim 25,
Wherein the position sensor comprises a DGPS (Differential Global Positioning System).
The method according to claim 1,
Wherein the moving object state measuring apparatus measures the velocity state of the moving object through at least one Doppler radar sensor (DRS).
The method according to claim 1,
The air-conditioning management apparatus includes:
A data collecting module for collecting the illuminance state of the airplane equal to the airplane equalization measured by the airplane equalization state measuring device and the velocity state of the moving object measured by the moving object state measuring device;
A power supply module for supplying electric energy to the air conditioner state measuring device and the moving object state measuring device;
A display module for displaying luminosity data and a light distribution graph of aviation equalization according to the distances of the aerial lighting equipments on a display screen; And
Wherein the control unit controls operations of the data acquisition module, the power supply module, and the display module, receives a speed condition of the moving object from the data collection module, calculates a distance from the airplane equalization to the moving object, Acquiring the distance data, converting the illuminance state of the aerial equalization provided from the data collection module to the luminous intensity data of the aviation equalization using the obtained distance data for aviation equalization, A control module for controlling the operation of the display module so as to convert the luminous intensity data of the aviation equalization according to the distance of the aviation equalization into the luminous intensity distribution graph and display the luminous intensity data on the display screen, The air-conditioning lighting system comprising: System.
The method according to claim 1,
The aviation equality management apparatus analyzes the luminous intensity data of the aviation equalization according to the distances of the aviation equalization to generate luminous intensity status information of the aviation equalization and stores the luminous intensity status information of the aviation equilibrium into a database And controls the operation of the display screen separately provided so as to be displayed and managed.
30. The method of claim 29,
The light intensity state information of the aviation equalization may include at least one of a maximum luminance information for aviation equalization, a minimum luminance information, an average luminance information, a luminance information based on an International Civil Aviation Organization (ICAO) standard, a vertical luminance information and a horizontal luminance information Wherein the at least one of the at least one air-to-air and the at least one air-to-
30. The method of claim 29,
The aviation equality management apparatus compares the luminous intensity status information of the aviation equalization according to the distance of the aviation equalization with a preset reference value range and determines whether there is an abnormality or not according to the comparison result, Wherein the control unit controls the operation of the air-conditioning system.

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