energies
Article Evaluation of Applicability of Various Color Space Techniques of UAV Images for Evaluating Cool Roof Performance
Kirim Lee 1 , Jihoon Seong 1, Youkyung Han 2 and Won Hee Lee 2,* 1 Department of Spatial Information, Kyungpook National University, Daegu 41566, Korea; [email protected] (K.L.); [email protected] (J.S.) 2 School of Convergence and Fusion System Engineering, Kyungpook National University, Sangju 37224, Korea; [email protected] * Correspondence: [email protected]; Tel.: +82-054-530-1492
Received: 13 July 2020; Accepted: 13 August 2020; Published: 14 August 2020
Abstract: Global warming is intensifying worldwide, and urban heat islands are occurring as urbanization progresses. The cool roof method is one alternative for reducing the urban heat island phenomenon and lowering the heat on building roofs for a comfortable indoor environment. In this study, a cool roof evaluation was performed using an unmanned aerial vehicle (UAV) and a red, green and blue (RGB) camera instead of a laser thermometer and a thermal infrared sensor to evaluate existing cool roofs. When using a UAV, an RGB sensor is used instead of expensive infrared sensor. Various color space techniques, namely light-reflectance value, hue saturation value (HSV), hue saturation lightness, and YUV (luma component (Y) and two chrominance components, called U (blue projection) and V (red projection)) derived from RGB images, are applied to evaluate color space techniques suitable for cool roof evaluation. This case study shows the following quantitative results: among various color space techniques investigated herein, the white roof with lowest temperature (average surface temperature: 44.1 ◦C; average indoor temperature: 33.3 ◦C) showed highest HSV, while the black roof with the highest temperature (surface temperature average: 73.4 ◦C; indoor temperature average: 37.1 ◦C) depicted the lowest HSV. In addition, the HSV showed the highest correlation in both the Pearson correlation coefficient and the linear regression analyses when the correlation among the brightness, surface temperature, and indoor temperature of the four color space techniques was analyzed. This study is considered a valuable reference for using RGB cameras and HSV color space techniques, instead of expensive thermal infrared cameras, when evaluating cool roof performance.
Keywords: UAV; cool roof; thermal images; color space techniques; surface temperature; indoor temperature
1. Introduction Temperature rises are intensifying with global warming worldwide. Abnormally high temperatures have occurred in Central Africa, Europe, the Middle East, Alaska, and South America [1,2]. Moreover, with the development of industries, the urban heat island phenomenon has occurred with urbanization, population increase, and vegetation reduction. The phenomenon is mainly caused by asphalt roads, concrete artificial structures, and high-rise buildings. The solar radiation reflected on building roofs raises the external surface temperature by up to 50 to 60 ◦C[3,4]. Such a structure has a bad effect on the living environment of people because it raises the temperature of the city, thereby causing problems for residential life and the cooling load [5]. In an effort to reduce the urban heat island phenomenon, research is being conducted to lower the surface temperature of building roofs.
Energies 2020, 13, 4213; doi:10.3390/en13164213 www.mdpi.com/journal/energies Energies 2020, 13, 4213 2 of 12
The building roof temperature is important because the building roof comprises approximately 20% to 25% of the city’s surface, and the energy consumption for cooling the city building is higher than that of non-urban buildings [6,7]. Cool roofs, rooftop greening, sprinkling treatment, solar power generation, and dual roofs, among others, are being investigated to reduce roof temperature [8–12]. Cool roofs are difficult to install because of structural problems and high installation and maintenance costs. White or light-colored paints that reflect well are applied to cool roofs using heat absorption from the color difference to reduce the heat accumulation in the roof. This can be easily applied to an existing building and is excellent in terms of cost because it is easy to install after the initial design, construction, and completion of the building [13,14]. Two previous studies on cool roof evaluation have been reported. First, evaluations according to environmental conditions, such as the material’s exterior wall thickness, thickness, roof condition, window insulation and size, and solar radiation energy, have been performed [15–19]. Second, only the roof surface temperature was evaluated; the external factors were excluded [20,21]. Satellite images, handle-type thermal infrared (TIR) images, and laser thermometers are frequently used in the existing method of roof surface temperature evaluation. Moreover, studies using unmanned aerial vehicle (UAV) infrared cameras have recently been conducted [22,23]. However, satellite images have a low spatial resolution; hence, the analysis of large areas is possible, and the local analysis is difficult. The handle-type TIR image and the laser thermometer have a disadvantage, in that obtaining the overall temperature of the rooftop surface is difficult, and the TIR camera for a UAV is expensive. To solve these shortcomings, a high spatial resolution is obtained, and the overall image acquisition of the roof surface is realized herein. The cool roof evaluation will be conducted using the RGB camera for a UAV instead of the TIR camera. Many studies have been conducted on the possibility of applying near-field monitoring because of the advantage of the UAV photogrammetry technique being able to obtain high-resolution images [24–26]. RGB cameras are cheaper than TIR cameras and can fly without restrictions in legal spaces, except for military areas; hence, you can obtain high-resolution images in cm and acquire the entire roof image. After applying various color space techniques to the image acquired by the RGB camera, we obtain the correlation between the roof surface temperature value of the TIR image acquired by a thermal infrared camera and the indoor temperature value obtained by a digital thermometer. The applied color space technologies are light-reflectance value (LRV), hue saturation value (HSV), hue saturation lightness (HSL), and YUV (luma component (Y) and two chrominance components, called U (blue projection) and V (red projection)). We evaluate the applicability of the cool roof evaluation by the color space technique through each correlation.
2. Materials and Methods
2.1. Study Area and Equipment The selected study area was the 9th building of Kyungpook National University Sangju Campus in Sangju, Gyeongsangbuk-do, Republic of Korea (Figure1). The colors used to evaluate the cool roof performance are as follows: (1) white, which is the most effective color in cool roof studies; (2) gray, which is similar to cement color; (3) green, which is most commonly used; (4) blue, which is used most often in factories; and (5) black, which absorbs the most sunlight. The gray color represents the color of the initial building. However, in the absence of maintenance, it is changed to dark gray or black; hence, black is added. Blue and green are waterproof paint colors mainly used only in South Korea. Overall, five colors were applied (Figure1). Energies 2020, 13, 4213 3 of 12 Energies 2020, 13, x FOR PEER REVIEW 3 of 12 Energies 2020, 13, x FOR PEER REVIEW 3 of 12
Figure 1. Study area (2559, Gyeongsang-daero, Sangju-si, Gyeongsangbuk-do, Republic of Korea). FigureFigure 1. StudyStudy area area (2559, (2559, Gyeongsang-daero, Gyeongsang-daero, Sangju-s Sangju-si,i, Gyeongsangbuk-do, Gyeongsangbuk-do, Republic Republic of of Korea). Korea). The red border represents the color for the cool roof performance evaluation. The five colors are The red border represents the color for the cool roofroof performanceperformance evaluation.evaluation. The The five five colors colors are are presented as capital letters: A: black; B: blue; C: gray; D: green; and E: white. presented as capital letters: A: black; B: blue; C: gray; D: green; and E: white.
Building No. 9 was chosen because the interior space of the fourth floor is divided equally, and Building No. 9 was chosen because the interior space of the fourth floor is divided equally, and the room indicated by the circle in the figure is not currently used. Hence, the experiment can be the room indicated by the circle in the figure is notnot currentlycurrently used.used. Hence,Hence, thethe experimentexperiment cancan bebe conducted under the same conditions (Figure2). conducted under the same conditions (Figure 2).
Figure 2. Floor plan of the study site. Figure 2. FloorFloor plan plan of of the the study study site. site. Building No. 9 has a few residents, and a few factors affect the surface temperature because no BuildingBuilding No. No. 9 9 has has a a few few residents, residents, and and a a few few fa factorsctors affect affect the surface temperature because no equipment is used for the experiment rooms, except for the outdoor unit on the rooftop. Figure 3 equipmentequipment is is used for the experiment rooms, except for the outdoor unit on the rooftop. Figure Figure 33 shows a room with indoor temperature measurements. showsshows a a room room with indoor temperature measurements.
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Figure 3. Fourth floor floor of building No. 9 used for the temperature measurement.
The UAV images were were acquired acquired herein herein using using Inspire Inspire 1, 1,which which can can fly fly for for up upto 18 to min 18 min using using the theremote remote sensing sensing technique, technique, while while the the RGB RGB images images for for applying applying the the color color space space techniques were acquired using a Zenmuse X3 camera. A Zenmuse XT630 TIR camera was used to measure the roof acquired using a ZenmuseFigure X3 3. Figurecame Fourth 3. ra.floor Fourth Aof buildingfloorZenmuse of building No. 9 used XT630 No. for 9 usedthe temperatureTIR for the camera temperature measurement was measurement .used .to measure the roof Figure 3. Fourth floor of buildingFigure 3.No. Fourth 9 used floor for ofthe building temperature No. 9 measurement used for the temperature. measurement. surface temperature for comparing and evaluating the color space technique. 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TableTable 1. UnmannedTable 1. TableUnmanned aerial 1. Unmanned vehicle aerial vehicle aerial(UAV (UAV), ( vehicleUAV), ) camera, camera(UAV), andcamera and digital digitaland thermometer digital thermometer thermometer specifications. specifications. specifications.specifications. Table 1. Unmanned aerial Tablevehicle 1. (UnmannedUAV), camera aerial and vehicle digital ( UAVthermometer), camera specifications. and digital thermometer specifications. UAV UAV RGB CameraRGB Camera Thermal ThermalInfrared CameraInfrared CameraDigital ThermometerDigital Thermometer UAV RGBUAV Camera RGB CameraThermalRGB Camera Infrared Camera Thermal Thermal InfraredDigital Infrared CameraThermometer Camera DigitalDigital Thermometer UAV RGB Camera Thermal Infrared Camera Digital Thermometer
(Inspire 1) (Inspire 1)(Inspire 1) (Zenmuse X3) (Zenmuse XT630) (Xiaomi) (Inspire 1) (Inspire 1) (Zenmuse X3) (Zenmuse(Zenmuse XT630) XT630) (Zenmuse X3) (Zenmuse(Zenmuse X3) XT630) (Zenmuse XT630) (Xiaomi) (Xiaomi) (Zenmuse X3) (Xiaomi) (Xiaomi) Weight 2935 g Resolution 40004000 × 30004000 × Resolution 640 512 (Inspire 1) Weight Weight2935 g(Zenmuse 2935Resolution g4000 ×X3)Resolution × Resolution4000 ×Resolution (Zenmuse 640 × 512XT630) 640 × 512× Temperature(Xiaomi) Weight 2935 g ResolutionWeight 2935 g ResolutionResolution3000 3000µ 640 × 512 Resolution 640µ × 512 Flight altitude Max: 4500 m Pixel size3000 1.561 1.561 m3000 Pixel size 17 m 0.1 ◦C Flight FlightMax: Max: 1.561× × 1.561 × display unit Flight Max: Flight Pixel1.561Max: size × Pixel 4000 size × Pixel1.561 size ×Pixel size 17 μm 17 μm WeightFlight time2935altitude Max: g 18 altitude minResolutionPixel4500 sizem 4500 FOV m 1.561PixelPixel 94 sizeμsizem◦ 1.561 Resolution μm 17 μmFOV Pixel size 640 45 ×◦ 51217Temperature37 μ ◦m Temperature altitude 4500 m altitude 1.5614500 μ mm 3000 1.561 μm Temperature× Temperature0.1 °C 0.1 °C Speed Max: 22 m/sMax: 18 Focal Max: length 18 3.61 mm Focal length 13 mmdisplay0.1 ° Cunit display unit 0.1 °C FlightMax: time 18Flight time Max:FOV 18 FOV 94° 94° FOV FOV 45° ×display 37° 45° unit× 37° display unit Flight Flight time Max: FlightFOVmin time min 94° 1.561 FOV×FOV 94°45° × 37° FOV 45° × 37° min min 25 C~+135 C PixelMax: 22 size Max: 22 PixelFocal size Focal − 17 ◦μm ◦ altitudeMaximum wind4500Max:Speed m 22 Speed FocalMax: length Focal1.56122 length 3.61μFocalm mm 3.61 mm Focal13 mm (High13 mm gain) TemperatureTemperature Speed 10 m/sFocalm/sSpeed length F-stopm/s3.61 mm Focal Flength/2.8 length3.61 13mm Scene mm length range 13 mm 0.3 C resistance m/s m/s length length 40 C~+550 C accuracy 0.1◦ °C Max: 18 −25 °C~+135−25 °°CC ◦~+135 °C ◦ display unit ± MaximumMaximum −25 °C~+135 °C − −25 °C~+135 °C Flight timeMaximum MaximumFOV 94° Scene FOV Scene (High gain) 45°(High (Low × gain)37° gain)Temperature Temperature minwind wind10 m/s 10 m/sF- stop F-stopScene F/2.8 F/2.8 (High gain) Scene Temperature(High gain) Temperature±0.3 °C ±0.3 °C wind 10 m/s F-windstop 10F/2.8 m/s F-stop rangeF/2.8 range− 40 °C~+550−40 °°CC ~+550 °Caccuracy±0.3 °C accuracy ±0.3 °C resistanceresistance range −40 °C~+550 °Crange accuracy−40 °C~+550 °C accuracy resistanceMax: 22 resistance Focal (Low gain)(Low gain) Speed Focal length 3.61 mm (Low gain) 13 mm(Low gain) 2.2. Unmanned Aerialm/s Vehicle (UAV) Data Acquisitionlength 2.2. Unmanned2.2. Unmanned Aerial Vehicle Aerial (VehicleUAV) Data(UAV Acquisition) Data Acquisition 2.2. Unmanned Aerial Vehicle2.2. Unmanned (UAV) Data Aerial Acquisition Vehicle (UAV) Data Acquisition −25 °C~+135 °C Maximum The UAV imagesThe UAV wereThe images UAV taken imageswere during taken were during taken the third duringthe third weektheScene week third ofof week August August of August 2018(High 2018 when 2018gain) whenthe when temperature the the Temperaturetemperature temperature was was was the wind The UAV10 m/simages were F-stoptakenThe UAV during images the F/2.8thirdwere weektaken of during August the 2018 third when week the of temperatureAugust 2018 waswhen the temperature was±0.3 °C highest and betweenthe highestthe 12:00 highestthe and and highest between and 13:00 between and 12:00 when between and 12:00 13:00the 12:00 and Sun when 13:00 and was range 13:00 the when Sun the when the washighest Sun the the − wasSun40 highest °C~+550 [ thewas27 , highest28 the[27 ]., °C28]. highest Moreover, [27Moreover,,28]. [27 accuracy,Moreover,28]. theMoreover, the photographs the the resistancethe highest and between 12:00 and 13:00 when the Sun was the highest [27,28]. Moreover, the photographsphotographsphotographs were taken were wereon taken a cleartaken on a day on clear a without clear day withoutday clouds without clouds(exte cloudsrnal (exte average rnal(exte averagernal temperature: average temperature: temperature: 31.1 °C 31.1; ° 31.1C; °C; were takenphotographs on a clear were taken day onwithout a clear day clouds without (external clouds (exte averagernal average temperature: temperature:(Low gain) 31.1 31.1 °C; ◦C; relative humidity:
60.4%; and wind speed: 0.69 m/s) to avoid the influence of shadows. Pix4D Capture, a UAV flight planning2.2. Unmanned software Aerial linked Vehicle to Google(UAV) Data Earth Acquisition and OpenStreetMap, was used to maintain a constant flight altitudeThe of UAV 70 m, images overlapping were taken 70% along during the the automatic third w flighteek of route August during 2018 the when data the acquisition temperature (Figure was4). Thethe UAVhighest flew and at thebetween lowest 12:00 speed and of 3 m13:00/s to when avoid thethe cameraSun was eff ects.the Ahighest total of[27,28]. 149 UAV Moreover, images were the acquired,photographs and were an orthophoto taken on wasa clear made day using without Agisoft’s clouds Photoscan. (external average temperature: 31.1 °C; relative humidity: 60.4%; and wind speed: 0.69 m/s) to avoid the influence of shadows. Pix4D Capture, a UAV flight planning software linked to Google Earth and OpenStreetMap, was used to maintain a
Energies 2020, 13, x FOR PEER REVIEW 5 of 12 constant flight altitude of 70 m, overlapping 70% along the automatic flight route during the data Energiesacquisition2020, 13(Figure, 4213 4). The UAV flew at the lowest speed of 3 m/s to avoid the camera effects. A5 total of 12 of 149 UAV images were acquired, and an orthophoto was made using Agisoft’s Photoscan.
Figure 4.4. FlightFlight course course over over the the study study area. area. The grayThe circlesgray indicatecircles indicate the location the oflocation the image of acquisition.the image acquisition. Lens distortion correction was performed before image matching using Agisoft’s Photoscan softwareLens [29distortion,30]. The correction model used was for performed the lens distortion before image correction matching was usin Brown’sg Agisoft’s distortion Photoscan model, whichsoftware was [29,30]. calculated The asmodel follows used (Equations for the lens (1) todistortion (6)): correction was Brown’s distortion model, which was calculated as follows (Equations (1) to (6)): y = Y/Z (1) y = Y/Z (1) q r = (x2 + y2) (2)
2 2 r = (x + y) 2 2 (2) x = x 1 + K 2 + K 4 + K 6 + K 8 + P r + 2x + 2P xy 1 + P 2 + P 4 (3) 0 1r 2r 3r 4r 2 1 3r 4r 2 2 y0 = y 1 + K r2 + K r4 + K r6 + K r8 + P1 r + 2y + 2P2xy 1 + P r2 + P r4 (4) 1 2 3 4 2 2 3 4 x = x 1 + K 2 + K 4 + K 6 + K 8 + P2 r + 2x + 2P1𝑥𝑦 1 + P 2 + P 4 (3) 1r 2r 3r 4r 3r 4r u = w 0.5 + cx + x0f + x0B + y0B (5) × 1 2