Color Plates

NREL

 

Best Research-Ce Efficiencies

 

image427

Thin-Film Technologies

 

image428
image004
image429
image430

VThin-film crystal

 

image431

VThin-film crystal

 

SunPower

(96x)

 

^28

 

image432 image433

о 24

 

UNSW.

 

image434

UNSW

 

Stanford

 

Variant UNSW

 

—-”■“■’’’University

So. Florida’ ARCO. Boeing

 

image435

T^^Photon Energy

,—“^ARCO і |nitoH c

 

Matsushita

 

Monosolar

 

Solarex

 

1 University of Maine

 

image436

image437

image438

(a)

 

Polycrystalline PV modules

 

Fixed-tilt PV arrays

 

image439

(c) 1-Axis tracking PV arrays
(d) Thin-film PV roof shingles

(e) Concentrating PV on 2-axis tracker (f) Building integrated PV

FIGURE 1.2 Examples of commercially available PV systems for producing electricity in a variety of applications: (a) fixed-tilt PV arrays; (b) polycrystalline PV modules; (c) fixed-tilt PV arrays; (d) thin-film PV roof shingles; (e) concentrating PV on 2-axis tracker; (f) building – integrated PV. (Courtesy of NREL Image Gallery, http://images. nrel. gov.)

image440
Wavelength (nm)

image441

FIGURE 1.3 Spectral response functions of selected PV materials illustrating their selective abilities to convert solar irradiance to electricity. (Courtesy of Chris Gueymard.)

Voltage

FIGURE 1.4 PV system performance characteristics determined by short-circuit current (T^) and open-circuit voltage (VOc), and maximum power point (Pmax).

Подпись: 6
image443

0 2 4 6 8 10 12 14 16 18 20 22

Voltage

Подпись: FIGURE 1.6 Combined effects of solar irradiance and array temperature on PV-array power output.

FIGURE 1.5 PV-array short-circuit current (Isc) is proportional to solar irradiance incident to the module. Open-circuit voltage is much less dependent on irradiance level.

Solar Irradiance (Watts / Square meter)

image445Parabolic trough collector

(b) Power tower and heliostats

MSJfc

аь.

(c) Dish Stirling engine (d) Linear Fresnel collector

FIGURE 1.7 Examples of CSP systems for converting high levels of DNI to heat and electricity (a) parabolic trough collector; (b) power tower and heliostats; (c) dish sterling engine; (d) linear Fresnel collector. (Courtesy of NREL Image Gallery, http://images. nrel. gov.)

Reflected Atmospheric

scattering

image446

FIGURE1.8 Solar-radiation components resulting from interactions with the Earth’s atmosphere and surface provide POA irradiance to a flat-plate collector (POA — Direct + Diffuse + Ground – reflected). (Courtesy of Al Hicks, NREL.)

image447

FIGURE 1.9 Time – series plot of solar-irradiance components for clear and cloudy periods as measured by pyrheliometers (A = DNI) and pyranometers (B = GHI; C =DHI), and corre­sponding sky images during the day, Golden, Colorado, July 19, 2012.

Solar Disk Radius

 

image448

1.0E+07

 

CD 1.0E+06

 

image449

image450

Подпись: СО 1.0E+05

Подпись: Field of View

The Eppley Laboratory, Inc. Model NIP (Normal Incidence Pyrheliometer) 1957 – 2012

Щ 1.0E+04

 

Circumsolar / Solar Disk = 24%

 

1.0E+03

 

NIP = 913 W/sq m Circumsolar / Solar Disk = 1.4%

 

1.0E+02

 

0.75

 

1.75

 

2.75

 

0.25

 

1.25

 

2.25

 

image453

Angle from Sun Center (Degrees)

Barstow, CA 7/29/77 14:23

 

■Atlanta, GA 6/29/77 11:58

 

FIGURE 1.11 Atmospheric aerosols increase the forward scattering of DNI, resulting in larger amounts of circumsolar radiation and affecting Sun shape. (a) Measurements from circumsolar – telescopes in California and Georgia and pyrheliometer fields of view. (b) Image during low – aerosol optical-depth conditions (~0.1) in Golden, Colorado. (c) Image during high aerosol loading (w 0.5) in Riyadh, Saudi Arabia.

 

image454

image455

FIGURE 1.12 Spectral distribution of solar irradiance above the atmosphere (extraterrestrial) and at the Earth’s surface after absorption by atmospheric gases (sea level), and the blackbody radiation corresponding to 5520 K temperature.

 

image456

FIGURE 1.13 Dependence of air mass on relative solar position with respect to an observer.

 

Подпись: Irradiance (W/m2/nm)

FIGURE 1.14 American Society of Testing and Materials (ASTM) standard solar spectra.

 

image458

image459

FIGURE 1.15 Elements of the solar-forecasting process for electric utility operational needs over a range of timescales.

Подпись: METEOSAT PRIME
Подпись: METEOSAT IODC

image462£} …………………………

Geqstationaryprbit

FIGURE 2.1 Geostationary and polar-orbiting satellite orbits and operational field of views.

FIGURE 2.3 Global map showing annual AOD 670 averaged over the year 2009, calculated from the Monitoring Atmospheric Composition and Climate (MACC) database developed by a consortium coordinated by the European Centre for Medium-Range Weather Forecasts (ECMWF). The color scale is 0.02-0.60.

FIGURE 2.4 Global map showing the annual average of precipitable water for the year 2009, calculated from the NOAA/NCEP Climate Forecast System Reanalysis (CFSR) database (kg/m2).

FIGURE 2.8 Sample of dynamic range for a site over the Atlantic Ocean from the visible channel of the GOES-East satellite. GOES-13 replaced GOES-12 in May 2010, resulting in a change in the dynamic range.

2012

І 100

FIGURE 2.11 Dynamic range for the year 2010 in a location with frequent occurrences of snow cover (Fort Peck, Montana).

FIGURE 2.12 Example of the classification output for Tartu-Toravere, Estonia, for Meteosat: (a) reflectance for the visible channel at 0.6 um, (b) classification for cloud-free land, (c) cloud-free snow, and (d) clouds. The x-axis represents day of year; the y-axis, time slot of the satellite image (bottom, morning; top, evening).

FIGURE 2.13 Snapshot of the SolarGIS database: annual average DNI (kWh/m2) representing years 1994 (1999 in Asia and Australia) through 2011.

0 200 400 600 800 1000 1200 0 200 400 600 800 1000 1200

FIGURE 2.17 Scatter-plot and cumulative frequency distribution of DNI data before (blue) and after (red) site adaptation for Tamanrasset, Algeria (grey): cumulative distribution of ground measurements.

(а)

Minutes Hours Days+

————————————– >

Forecast Lead Time

FIGURE 3.1 (a) Conceptual diagram of forecast skill hand-off as a function of forecast lead time

for different methods ranging from persistence to climatology. The curve with the greatest potential for advance in skill is numerical weather prediction; satellite data play a vital role here in terms of both analysis and improved parameterization. (b) Example solar-forecast methods from Fig. 3.1a, from left: persistence, surface-based trajectory, satellite-based trajectory, weather – forecast models, and climatological cloud statistics constrained by meteorological regime. Satel­lite information is applicable to all of these timescales.

FIGURE3.5 Cloud advection in a short-range solar forecast. Top: surface observation time series of solar irradiance as measured at a surface station near Fort Collins, Colorado, on June 26, 2010. Middle: clouds (blue — cold tops, yellow — warmer tops) moving across the station location (shown as a white cross). Bottom: cloud field over the solar array as viewed from the south. Over the 2100-2130 UTC time period, a break between clouds results in a rapid ramp-up of solar irradiance.

Time (UTC)

FIGURE 3.7 CloudSat cross-section through the eye of Hurricane Ileana in the Eastern Pacific on August 23, 2008, showing the detailed inner-core structure of the storm.

N0GAPS* Pressure (mb)

FIGURE 3.8 Importance of accounting for cloud height and solar geometry when forecasting solar irradiance at surface stations. Shadows may extend tens of kilometers away from the sub­cloud location.

FIGURE 3.9 Speed and directional sheer of the atmospheric wind field—an important consid­eration for cloud advection that requires detailed knowledge of the vertical distribution of clouds.

FIGURE 3.10 Observed and simulated cloud field (Weather Research and Forecasting (WRF) model data passed through an observational operator).

January 1998-2002 Valid Time: 1900 UTC

500

FIGURE 6.2 Dispersion-smoothing effect occurring at 25 locations dispersed over a 4 x 4 km area (Data from the Cordelia Junction network, San Francisco Bay area, California.)

FIGURE 6.3 Site-pair correlation as a function of distance (D) and time interval (At) for stations in the ARM network. (From Mills and Wiser 2009.)

FIGURE 6.4 Site-pair variability correlation as a function of distance derived from hourly 10 km-resolution satellite data for California (top) and the Great Plains (bottom). The top row in each case represents p as a function of distance. The bottom row expresses this relationship as a function of the ratio between D and At x implied CS, showing that the distance relationship is predictably dependent on At and CS.

Б50

10 20 ЗО 40

At (minutes)

FIGURE 6.7 Applying equation 6.4 to estimate the effective site-pair decorrelation distance as a function of Dt and CS. The short line labeled “Virtual network” represents the preliminary estimate of this relationship based on limited evidence.

FIGURE 6.10 Smoothing effect at the scale of a metropolitan area comparing single-site and modeled 40 km x 40 km extended fluctuations for different timescales.

Time

CRITICAL TIME SCALE

RR0 [(MW*arbitrary scaling factor)/1 s]

RR0 [(MW*arbitrary scaling factor)/10 s]

RR0 [(MW*arbitrary scaling factor)/30 s]

RR0 [(MW*arbitrary scaling factor)/60 s]

FIGURE 7.7 Cumulative distribution of ramp rates in power output for the 1 y period from August 1, 2011, through July 31, 2012. Ramp rates are shown at various timescales: 1 s (top left), 10 s (top right), 30 s (bottom left), and 60 s (bottom right). At each timescale, shown are the ramp rates of measured power output (thick blue line), WVM run with ground CS values (dashed green line), WVM run with NAM-cdf CS values (dashed red line), and a point sensor with no smoothing (dashed magenta line). The x-axis is the RR in MW/timescale multiplied by an arbitrary scaling factor to protect the confidentiality of the power data.

timescale

September, 2012

Sun Mon Tues Wed Thurs Fri Sat

FIGURE 7.10 RRs for the 60 MW plant: violations (red dots); total number of violations per day (bottom, bold red).

days per month

10% 15% 20% 25% 30% 35% 40% 45% 50%
RR [% of capacity / minute]

Longitude (Degrees)

FIGURE 8.1 Forecast GHI (W m-2) on April 10, 2010, at midday from the North American Mesoscale model (NAM).

FIGURE 9.1 TSI mounted on an inverter enclosure at a solar plant in the United States.

FIGURE 9.2 (a) Canopy camera and (b) the SIO-MPL’s WSI deployed at the Department of

Energy’s Atmospheric Radiation Measurement Program field site in Lamont, Oklahoma.

FIGURE 9.6 HDR process on the USI showing three exposure times: (a) 5 ms, (b) 20 ms, and (c) 80 ms; (d) final composite.

Subset of pixels
to correlate

Search Window

Position of
original subset

region with
highest correlation!

FIGURE 9.13 Normalized cross-correlation method used to compute inter-image cloud motions. The image at to-30 s (a) is broken into small tiles, each of which is cross-correlated with the corresponding search window in (b), the image at fo.

FIGURE 9.17 Sequential cloud advections for a single forecast issue with the direction of motion indicated. The cloud positions are shown for the nowcast (a), along with the 5 min (b), 10 min (c), and 15 min (d), cloud-position forecasts.

cloudmap

shadowmap

FIGURE 9.18 Ray tracing to construct a georeferenced mapping of shadows. The shadow value for a given point in the forecast domain grid is determined by tracing a ray along the solar vector and determining the cloud value at the intersection with the cloudmap.

solar anywhere

/iNHANCCO RISOLUTION

SOLAR anywhere

/STANDARD RISOLUTION

Zoom in lo select location(s)

Standard Resolution
Hourly – 10 km

Enhanced Resolution
/2 hourly – 1 km

FIGURE 10.3 KSI and OVER metrics. Top: modeled and measured cumulative probability distributions and the critical value envelope around the measured distribution. Bottom: absolute difference between the two distributions. The metrics are obtained by integrating the area under the curves: KSI (lightly shaded); OVER (striped).

RMSE (Wm

FIGURE 10.4 Annual RMSE and forecast skill as a function of forecast time horizon.

Forecast Skill

FIGURE 10.5 Comparison of hourly forecasts and persistence versus measured GHI scatter plots for 1, 3 h ahead and 1,3 d ahead. Scatter plots provide a qualitative, visual appreciation of model performance showing that the core of forecast points are closer to the 1:1 line and exhibit fewer outlying points.

FIGURE 13.5 Transform between (a) lognormal and (b) Gaussian spaces and its implications. The horizontal blue, red, green, and magenta lines indicate the inverse transform from the transformed normal distribution back to the lognormal distribution for lognormal distributions of s = 0.25, 0.5, 1.0, and 1.5, respectively. When inverted from the Gaussian-transform analysis space, the transform approach finds the median in the lognormal space and thus loses all skewness information contained in the original lognormal distribution, where the vertical blue, red, green, and magenta lines indicate the respective original lognormal modes.

FIGURE 13.6 Cloudy-radiance assimilation using the RAMDAS 4DVAR system for a region in central Oklahoma with a domain of 300 x 300 km (using 6 km horizontal grid spacing). The results demonstrate use of the GOES Sounder channel-1 (12 pm) on March 21, 2000, at 11:45 UTC. Blue denotes cold cloudy brightness temperatures (K) (i. e., high to middle clouds); red denotes warm brightness temperatures (K) (i. e., low clouds). The DA processing moves from left to right: (a) first guess (current model state), (b) final assimilation analysis state, and (c) GOES Sounder-channel 1 satellite observations. The original mean RMS error was 39 K; in the converged final analysis, the RMS error is 3.9 K. (Images courtesy of Manajit Sengupta.)

FIGURE 14.3 Percentage maximum total revenue (R) as a function of forecast error and the ratio of RTM to DAM price for a market system with a forecast-deviation penalty of twice the maximum of the RTM or DAM (equation 14.3). The white Hue represents 0 total revenue, not including cost of operation.

FIGURE 14.6 Direct cloud assimilation using a GOES cloud mask. (a) Clouds are to populate qvapor in WRF initial conditions (green); (b) May 17, 2011.

FIGURE 14.9 GOES satellite imagery: (a) June 11, 2011, compared to the intraday (0-24 h, initialized on June 11, 2011, 12 UTC) (b) and day-ahead (24-48 h, initialized on June 10, 2011, 12 UTC); (c) WRF-CLDDA irradiance forecasts in San Diego, California.

[1] Of course, this assumption, like most other model assumptions, becomes less robust for very large solar-zenith angles

[2] Current U. S. GOES satellites provide images on a half-hour basis, whereas current Meteosat satellites provide data every 15 min. The next round of GOES satellites is expected deliver data every 5 min.

[3] Concerns with calibrations at three of the Texas sites and the three component comparison inconsistencies (GHI, DNI, and DHI) skewed the results, so all the Texas sites were removed and the MBE errors were recalculated with a more consistent dataset. These errors are discussed more in the measured data section of this chapter.

[4] Direct normal rradiance (DNI) would be the relevant quantity if concentrating technologies were considered.

[5] The range of the global index is reduced as the Sun’s elevation decreases, because the relative weight of diffuse irradiance increases during clear-sky conditions.

[6] Currently available in North America.

Solar Energy Forecasting and Resource Assessment. ISBN: 9780123971777

Copyright © 2013 Elsevier Inc. All rights reserved.

[7] Kt* equals the ratio between (satellite-derived) GHI and local clear-sky global irradiance

GHIclear.

[8] The current version of SolarAnywhere uses only the satellite’s visible channel to determine cloud indices; hence, cloud motion can be determined only after sunup. As a result, N-h forecasts are only available N + 1 h after sunrise. The new version of SolarAnywhere uses the infrared satellite channels in addition to the visible channel, thus making it possible to infer nighttime cloud motion and so overcome this limitation.

[9] The achievable time resolution is defined by the ratio of cloud speed to the image’s spatial resolution (1 km), which defines the size of the cloud structures that can be captured to determine variability at a given time scale.

[10] Therefore, the results here represent a worse-case evaluation of the SolarAnywhere forecasts because, operationally, forecasts are refreshed every hour.

[11] Note that another measure of dispersion, mean absolute error, was recently recommended as the preferred methodology to report relative (percentage) errors (Hoff et al. 2012).

[12] This is because the satellite model used in this evaluation uses only the satellite’s visible channel. The next version of SolarAnywhere, which uses the satellite’s IR channels, will not have this limitation.

[13] The loss of dynamic range reflects the tendency of the NDFD forecasters to increasingly “hedge” their forecasts as the time horizon increases.

[14] Note that the IEA team did not compare the GFS global model directly to the other global models, but only its application via mesoscale models or the NDFD. Mathiesen and Kleissl (2011) have shown that the standalone GFS model should indeed perform better than through-the-filter mesoscale models, which tend to introduce unwarranted dispersion error at this stage of their irradiance-modeling development.

Updated: August 25, 2015 — 11:06 am