Networks of meteorological surface stations in the U.S.
are exemplified, in the synoptic scale by the NWS-FAA-DoD Automated Surface
Observing System (ASOS) (NOAA, 1992), and in the mesoscale by the NCAR
Portable Automated Mesonet (PAM) (Brock and Govind, 1977 and Brock et al.,
1986) and the Oklahoma Mesonetwork (Mesonet). These networks are characterized
by slow response instrumentation (no flux measurements) and short towers
(10 m or less). These three networks will be described in the following
text. ASOS, PAM and the Mesonet were designed to meet quite different objectives.
This is reflected in the design philosophy, site selection criteria, communications
systems, power sources, measurement site configuration, instrumentation
and local data processing employed. This section ends with a brief overview
of data quality assurance procedures.
PAM is a research-oriented mesoscale system. It was designed to support short-term, intensive research projects. A typical term was one to three months. The scale ranged from locating 30 stations in 1 km2 to 60 stations spread out over two states. There were two PAM systems and soon there may be a third. PAM I was used from 1976 to 1982 and PAM II was used from 1985 to 1993. As the name suggests, PAM was designed to be portable, readily moved from one area of the county to another. This meant that set-up time had to be short; crews could install 3-5 stations per day. It also meant that neither commercial power not telephone communications could be used.
The Mesonet is the largest and most comprehensive of the
state networks (Meyer and Hubbard, 1992). It provides 108 stations distributed
across the state of Oklahoma. It is designed to support agricultural, hydrological
and meteorological goals as well as emergency management and energy conservation
needs. Design of the Mesonet was constrained by cost, available data communications
systems and above all, by the need to use rural sites. The cost and site
constraints meant that, in contrast to the ASOS, the Mesonet could not
use commercial power or telephone communications. They were generally not
available at the preferred sites and it would have been prohibitively expensive
to bring them in.
Research investigations employing PAM had various objectives, time durations, and terrain types. Criteria for site selection changed accordingly. PAM stations have been located from sea level to nearly 4000 m, in deserts, grasslands and forests. Sometimes they were located in valleys precisely to monitor the valley effect.
Mesonet site standards were established considering the diversity of potential applications. Rural sites were required to avoid anthropogenic factors present in urban and suburban sites and to make the sites representative of agricultural applications.
Physical characteristics of a site, including soil properties, must be representative of a large area. Since the USDA Soil Conservation Service has conducted extensive surveys of the soil types in the state, soil types characteristic of each region were known. The Soil Conservation Service will determine soil types at each Mesonet site to a depth of 1 m. Sites were required to be as far away as possible from irrigated areas, lakes and forests to minimize those influences.
Site slope was specified to be less than 5o. There should be a minimum of obstructions that impede ventilation. The rule of thumb is that the distance between a wind obstruction and the site should be at least 20 times the height of the obstruction (Fujita and Wakimoto, 1982, and Wolfson and Fujita, 1989). Precipitation measurements are best made in clearings surrounded by brush and trees to reduce the wind effect. This conflicts with the requirement for good ventilation. To minimize land use the rain gauge was located near the tower. The good ventilation requirement prevailed, i.e., priority was given to wind exposure at the expense of an ideal precipitation measurement site. To partially compensate for this, each rain gauge is equipped with a wind screen, as described below.
Each site must be accessible by vehicle in all weather. Vegetation at the site should be uniform and low. Short grasses were preferred. Bare soil should not be visible except where that is a characteristic of the surrounding region.
Other essential requirements included a reasonably uniform distribution of sites over the state, with at least one site in each county. There was a stringent communications requirement that will be discussed below. Land owners were asked to provide the site free of charge. Site security was an additional constraint; the sites were selected to minimize the probability of vandalism, if possible. However, there was no requirement to locate sites near telephone or power lines.
In the real world, some of these requirements are mutually exclusive and so many sites failed to meet all of the above specifications. Finally, all sites are documented with photographs to show the terrain, especially the wind fetch. Fig. 8.1 shows the locations of the 108 Mesonet sites:


Two-way communications and much longer message lengths
were deemed essential for the Mesonet so it does not use GOES. And the
Mesonet will be fully operational by the time the next GOES has been put
into orbit.
OLETS is an ideal vehicle for the Mesonet communications traffic as it provides the reliability, bandwidth and full two-way services needed (Crawford and Long, 1993). The Mesonet message load represents only a small fraction of the OLETS system capability. To get data to OLETS, the Mesonet had to provide a direct radio link from each remote site to the nearest OLETS terminal, typically in a sheriff's office or police station. The resulting communications system is shown in Fig. 8.3. An RF base station, located at the chosen OLETS terminal, is capable of servicing several remote sites directly, or through repeaters.

By using a combination of direct radio and OLETS, the
Mesonet gained considerable flexibility. It was possible to cover the whole
state but sites had to be in line-of-sight range of an OLETS terminal or
a repeater. It is possible that communications will be disturbed occasionally
by inversion ducting or interference from other transmitters.
Systems, such as PAM and the Mesonet, which must use alternate power sources are constrained to select sensors with low power consumption and then to switch the sensors on only as needed to further conserve power. Usually, sensors must operate from an unregulated supply (typically 10 to 30 V). Heaters are not available and local computational capability is severely limited. Therefore, all components must be rated for operation over the temperature range of -30 to 50oC.
PAM and the Mesonet use a solar power system comprising
a solar panel, a regulator, a battery and an enclosure. In the Mesonet,
the data logger, the modem, transceiver and the sensors consume less than
1 W. The battery and solar panel were sized to provide this level of power
for a minimum of 10 days under the worst expected conditions (continuously
cloudy and cold) in Oklahoma.

Fig. 8.5 shows a PAM II station. The 10 m mast is self-supporting; no guy wires are required. The tripod was simply staked down. This meant that no site preparation was required (no concrete pad needed), set-up and tear-down could be accomplished quickly. The wind sensors were at the top of the mast, at 10 m.

The layout of a Mesonet remote station is shown in Fig. 8.6 and in Fig. 8.7. The lightning rod, shown in Fig. 8.6, is used at only 27 of the 108 sites. This reflects some uncertainty as to the need for lightning rods in Oklahoma. Perhaps after a decade of operation we will know whether they were needed.


The data logger enclosure is not shown. It contains the data logger, the RF modem, the radio transceiver, and the barometer. The radio transmits in the VHF range at 169.425 MHz with an RF power output of 5 watts.
The pyranometer is mounted on a free standing tripod south of the tower so that there would be good access to the pyranometer for cleaning and to minimize reflections from the tower. There are two soil temperature plots, one for sensors installed under bare soil and one for sensors installed under native sod cover.
The towers are guyed so a concrete base was not needed. A galvanized iron tower was selected for low cost. Aluminum towers are much lighter and easier to transport but, because of their higher cost, they are justified only if a tower is to be moved frequently. The wind sensor is mounted on the top of the tower. Temperature and relative humidity sensors and the 2 m wind sensor are mounted on booms projecting about 1 m from the tower.
Due to the frequent presence of livestock, the stations
are enclosed by a cattle panel fence approximately 10 m by 10 m. This protects
the tower, the guy wires, the rain gauge and wind screen, the soil plots
where soil temperature measurements are made and the pyranometer stand.
| Variable | Number | Sensor | Range | Inaccuracy1 |
| Cloud height |
|
Laser ceilometer | 30...3700 m | |
| Visibility |
|
Forward scatter meter | < O.4...16+ km | up to |
| Present weather
precipitation identification |
|
LEDWI2 | Detect light, moderate,
and heavy rain or snow; or mixed precipitation |
0.25 mm or 10% |
| Freezing rain
occurrence |
|
Vibrating element | Accumulation over
0.25 mm/hr |
1% in precipitation
rates as low as 1.3 mm/hr |
| Ambient
temperature |
|
Resistive
temperature device (RTD) |
-600C...540C | RMSE
0.5oC...1.0oC |
| Dew point |
|
Chilled mirror | -340C...300C | RMSE
O.60C...4.40C |
| Pressure |
|
Redundant aneroid cells | 570...1060 mb | 0.7 mb |
| wind direction |
|
Vane | 0...359o | |
| wind speed |
|
Cup anemometer | 0.. .60 m/s | |
| Liquid precipitation |
|
Heated tipping
bucket |
0...250 mm/hr | 4% of hourly total |
Each PAM station measures wind speed and direction, temperature
and relative humidity, pressure and rainfall. The stations can be readily
expanded to measure many other parameters. The PAM data are reported at
5-minute intervals.
A Mesonet remote station includes a 10 m tower, a suite of sensors, a solar power system, a data logger, an RF modem, a transceiver and an antenna are enclosed in a fence for protection from livestock and other animals. Every station is equipped with a standard set of core sensors. In addition there are a number of supplemental sensors that are installed on about half the stations. The sensors are listed in Table 8.23.
|
|
|
|
|
| [Core Sensors: (All Stations):] | |||
| Propeller-vane
Wind speed and direction |
R. M. Young 5103 | 10 m | Speed: 1 to 60 m/s
Direction: 0 to 360o |
| Air temp. Thermistor &
Sorption humidity sensor Radiation shield |
Vaisala HMP35C
Coastal Climate |
1.5 m | Air temp: -30 to 50oC
Humidity: 0 to 100% Unaspirated 12-plate type |
| Barometer | Vaisala PTB202 | 0.75 m | 700 to 1100 mb |
| Rain gauge
Wind screen |
MetOne 099M
Internal constr. |
0.6 m | Tipping bucket 30 cm gauge.
0.25 mm bucket Alter style |
| Pyranometer, insolation | LiCor 200 | 1.8 m | Silicon cell |
| Thermistors (2) soil temp.4 | Fenwal | -10 cm | -30 to 50oC Stainless steel jacket |
| [Supplemental Sensors (About 50 stations):] | |||
| Thermistors (3)
Soil Temperature |
Fenwal | -5 cm
-30 cm |
-30 to 50oC Stainless steel jacket |
| Thermistor, Air Temp. &
Radiation shield |
Thermometrics
Coastal Climate |
9 m | -30 to 50oC, fast response
Unaspirated 12-plate type |
| Cup anemometer | R.M. Young 3101 | 2 m | Speed 0.5 to 50 m/s |
| Leaf wetness sensor | Internal constr. | 0.5 m | Electrical impedance grid |
Inaccuracy and resolution are listed for each sensor in
Table 8.3. The inaccuracy specification was provided by the instrument
vendor. It does not include errors due to insufficient coupling with the
atmosphere. As noted below, air temperature sensors can have large radiation
induced error due to the radiation shield. Resolution is that of the data
in the Mesonet archive. It is determined, in most cases, by the resolution
of the analog-to-digital converter in the data logger. Resolution is listed
here because there are applications which can reasonably use some of this
resolution, even though it is far smaller than the accuracy specification.
For example, the barometer can detect gravity waves. A gravity wave of
0.1 mb amplitude could be detected and the amplitude measured even though
the inaccuracy of the sensor is 0.4 mb.
|
|
|
|
|
| [Core Sensors: (All Stations):] | |||
| Wind speed and
Direction |
2% of Reading
3o |
0.03 m/s
0.05o |
|
| Thermistor, air | 0.35oC | 0.01oC | |
| Humidity | 3% | 0.03% | |
| Barometer | 0.4 mb | 0.01 mb | |
| Rain gauge | 1% of reading | 0.25 mm | |
| Pyranometer, insolation | 5% of reading | 0.23 W m-2 | |
| Thermistors, soil | 0.5oC | 0.03oC | |
| [Supplemental Sensors (About 50 stations):] | |||
| Thermistors, soil | 0.5oC | 0.03oC | |
| Thermistor, Air | 0.4oC | 0.03oC | |
| Cup anemometer | 2% of reading | 0.25 m/s | |
| Leaf wetness sensor | (not established) | ||
PAM and the Mesonet do not measure cloud height, visibility,
present weather or freezing rain. The ASOS does not measure solar radiation,
soil temperatures or leaf wetness.
The ASOS visibility sensor is a forward scatter meter. It uses visible (mostly blue) light from a pulsed Xenon flash lamp. An optical detector observes a portion of the beam from an angle of about 400 from the center of the beam. No light from the beam will reach the detector unless there are particles in the beam which scatter the light out of the beam and into the detector. The advantage of the short path is that the source and detector can be mounted to a common, rigid frame and thus preserve their respective alignment. Further, it is easier to monitor the source strength. The primary disadvantage is that the instrument can be seriously affected by local variations in visibility such as a patch of fog. This is countered by averaging over time. The instrument is sampled once every 30 s and the measurement is converted to an extinction coefficient which, in turn, can be converted to visibility. A one-minute mean is calculated from the 30 s data. Then a 10-minute harmonic mean is calculated from the 1-minute data and updated every minute. The harmonic mean given by
| (8.1) |
The detector output is filtered into two band-pass regions. The low band is 75 to 250 Hz while the high band is 1 to 4 kHz. Signal power is measured in each band. Rain/snow discrimination is determined from the ratio of power in the high band to that in the low band. Rain falls faster than snow and produces more power in the high band. For a given precipitation type, such as rain, the scintillation frequency is proportional to the vertical fall speed which, in turn, is a monotonic function of the particle diameter. Thus the power in the band is related to the precipitation rate. While the tipping-bucket rain gauge rain rate is the one reported by the ASOS, the LEDWI rate can be used to indicate precipitation intensity on a coarse scale: light, moderate, heavy.
Fog, dust and smoke move with very small vertical speeds
so don't affect either band. When blowing snow is carried to a height greater
than the LEDWI, about 3 m, the instrument can mistakenly report falling
snow. Ice pellets may be reported as rain.
The cylinder is oriented vertically to avoid false bird
signals. Snow can accumulate on the probe when the temperature is near
freezing and generate a false signal. Snow can be differentiated from freezing
rain by checking the output of the LEDWI.
The primary wind sensor of the Mesonet is the R.M. Young Model 5103 Wind Monitor which is a propeller, wind vane combination. It is mounted at the World Meteorological Organization (WMO, 1983) standard height of 10 m above ground level.
Sensor specifications were selected to balance cost, performance and durability. The wind speed sensor, a propeller, has a starting threshold of 1 m/s, a range of 0 to 60 m/s, with gust survival to 100 m/s, and a distance constant of 2.7 m. The signal output is a magnetically induced a.c. voltage which produces 3 cycles per propeller rotation or 10.2 Hz per m/s. The vane threshold is 1.0 m/s, the damping ratio is 0.25 and it has an undamped natural wavelength of 7.2 m. See ASTM, 1987 for a definition of these terms and for methods of testing wind sensors. The associated transducer is a pot which has a range of 0 to 355o (with 5o open). The propeller vanes are oriented to true North.
Local processing, in the data logger, generates six products from these two measurements: average wind run, average vector wind speed and direction, standard deviation of both wind speed and direction, and the maximum wind speed within the averaging period. These measurements are expected to be in compliance with the emerging standard for wind measurement to be issued by the Federal Coordinator for Meteorology (private communication with Thomas Lockhart).
Some stations have a cup anemometer at the 2 m level.
This anemometer has a starting threshold of 0.5 m /s a range of
0 to 50 m/s with gust survival to 60 m/s, and a distance constant
of 2.3 m. The signal output is a magnetically induced AC voltage which
produces 1 cycle per cup wheel rotation or 1.33 Hz per m s-1.
A RTD is mounted in the mirror, as close to the front surface as possible, to measure the mirror temperature. The assumptions are that the RTD is at the mirror front surface temperature, that the RTD is properly calibrated, and that the mirror is being held at the dew point by the controller. The latter assumption fails when there is dirt on the mirror, when there are salts on the mirror, and when the ambient dew point changes faster than the controller can change the mirror temperature. Dirt on the mirror can cause light scattering which may confuse the photodiode signals. This is controlled by activating an automatic mirror cleaning procedure once a day. In this procedure, the mirror is heated to drive off all of the moisture. As the condensate drops evaporate, their radius shrinks and dirt particles held within the drops are pulled together. When the mirror is dry, the dirt particles will be in small, isolated clumps and will have little effect on the reflected light. Salts on the mirror can act as condensation nuclei, reduce the vapor pressure around the drops and cause dew to form at a higher temperature than the true dew point. Conversely, if the mirror is too clean, dew may form at a temperature lower than the true dew point. Therefore, while the chilled-mirror dew point instrument seems to be a direct implementation of the dew point definition, there are a number of ways that it can be in error.
PAM used a specially designed psychrometer for humidity measurements for years and than gradually moved to sorption sensors. In the early years of PAM, sorption sensors were not nearly as good as they are today. Most PAM projects that required accurate humidity measurements were summer projects. The psychrometer, shown in Fig. 8.8, was designed for continuous operation with a double water bottle that could keep the wick moistened for a week even in very dry weather.

The advantage of a psychrometer is that the sources of error have been well documented and are readily controlled, as noted below:
Ventilation rate. Typically, the ventilation rate should be at least 3 m/s to maximize the heat transfer by convection and evaporation and to minimize heat transfer by conduction and radiation. The minimum ventilation rate needed is a function of the sensor thermal mass. Sensors made from small diameter thermocouple wire with a fine cloth wick have been successfully used without forced ventilation (Stigter and Welgraven, 1976.)
Radiation incident on the temperature sensors. The sensors must be shielded from direct and reflected solar radiation and from long-wave or earth radiation. This is a major source of error in the field that is not usually a factor in the laboratory.
Mesonet air temperature and relative humidity are measured
at 1.5 m with a combination thermistor-sorption probe mounted in an unaspirated
multiplate radiation shield. The sensor is a HMP35C
probe which is a Vaisala HMP35 sorption probe for humidity modified by
Campbell Scientific to include a thermistor for air temperature and a power
switching transistor to reduce power consumption. Relative humidity is
sensed by a capacitive sorption sensor with a range of 0 to 100% RH, and
errors of
2% for 0 to 90% and
3%
in the range 90 to 100%. The air temperature and the humidity sensor are
enclosed in a filter to keep dust off of the humidity sensor. This has
the effect of slightly reducing the air flow around the sensors and therefore,
increasing their time constant. This can be significant in light
winds, perhaps increasing the time constant to as much as 10 minutes.
Since the temperature sensor is in close proximity to the humidity sensor, the relative humidity output can be readily converted to dew point, which is more useful for many applications. Conversion of a constant 2% relative humidity error to dew point error is nonlinear and is a function of the ambient air temperature, as shown in Fig. 8.9. The Mesonet maximum tolerable humidity error goal was specified in terms of dew-point temperature. The specified error was <0.1oC for dew points above 0oC; the tolerance is somewhat larger for lower temperatures as shown by the dashed line in Fig. 8.9. A 2% error in relative humidity, when converted to a dew point error, meets this goal except when the dew point depression is large. For example, when the air temperature is 30oC, the sensor dew point error is less than 1.1oC when the dew point is greater than 10oC, or the dew point depression is less than 20oC.

In general, an aspirated air temperature sensor is superior to one mounted in a passive radiation shield; errors in a passive shield can be as large as several degrees Celsius in calm wind (< 1 m/s) and strong radiation (> 800 W m-2) conditions. Extreme conditions of insolation coupled with a highly reflective ground surface were used by Gill (personal communication with R. M. Young) to obtain the data shown in Fig. 8.10. The upper curve in Fig. 8.10 shows the effect of a sun angle approximately 70o above the horizon with an irradiance of 1080 W m-2. The lower curve is for the same intensity but with a sun angle of 90o above the horizon. Evidently the shield is more sensitive to radiation coming from an angle of 70o, probably due to internal reflections. This figure cannot be used to correct Mesonet air temperature data because the plotted data were obtained in a wind tunnel under conditions not necessarily representative of actual sites and because the Mesonet radiation shields are similar to the Gill shield but not exactly the same. However, the figure can be used to indicate conditions of light winds and strong radiation when the Mesonet air temperatures should be used with caution.

A passive shield was specified, with some reluctance,
because of power and cost constraints. Calm winds and a strong radiation
combination is somewhat less frequent in Oklahoma than in other parts of
the country. The ideal solution would be an aspirated shield designed to
be an efficient radiation shield even when the fan
is turned off. Then the fan could be turned on only when needed. Until
such a shield is available, the Mesonet may flag the air temperature data
as questionable when the ambient wind and radiation conditions are not
favorable. It should be noted that an aspirated shield is not necessarily
free from radiation induced error.
Some of the Mesonet stations have another air temperature
sensor at 9 m. It is a thermistor identical to the one described above
and has the same type of radiation shield.
The barometer selected for the Mesonet was the Vaisala PTB 202 which utilizes a silicon capacitive integrated circuit sensor. To minimize power consumption, the barometer is switched on only when needed to make a measurement. The sensor range is from 700 to 1100 mb with an uncertainty of 0.4 mb. This is an acceptable error level for pressure measurement given the range of pressures and temperatures (-30 to 50oC) to which the barometer is exposed. This does pose a problem for those wishing to compute pressure gradients over small horizontal distances, as illustrated in Fig. 8.11, which shows the geostrophic wind error due to using barometers with a given level of uncertainty. For example, if the pressure gradient between two stations, separated by 30 km, was in error by 0.4 mb, the error induced into the geostrophic wind would be 13.3 m/s. Another source of error, which can be even larger, is due to correction of the station pressure to a reference height. There is some uncertainty in the actual station height (where an 8 m height error is approximately equivalent to a 1 mb pressure error) and the correction algorithm may introduce another uncertainty. Any computation of pressure gradients must be made with great care keeping these error sources in mind.

Ideally, the station pressure is the total static pressure uncontaminated by the dynamic pressure due to wind flow. The classical way to minimize dynamic effects is to use a static pressure port which is usually some sort of flat plate with a hole, or static port, in the middle connected to the barometer with a tube. The ASOS barometer is located inside a building and is simply vented into the building unless the building is pressurized. In that event, the barometer is vented by a tube to a static pressure port outside of the building.
The PAM static port is mounted on a boom projecting out
about a meter from the tower. One of the problems with a flat-plate port
is that if it is not horizontal, perhaps due to accidental misalignment,
large errors can be induced. An alternative, used in the Mesonet, is to
run the pressure tube from the barometer down the tower leg to a point
about 15 cm above the ground and to terminate it there with a filter to
keep insects out. This is a compromise since the average wind speed is
only truly zero at ground level, but there the tube would be subject to
flooding and possible mechanical damage.
The objective in the Mesonet is to measure rainfall rather
than precipitation. This distinction is made in recognition that the sensor
chosen, an unheated tipping bucket gauge, is not suitable for snow or freezing
precipitation measurement. Cost and power considerations dictate the use
of an unheated gauge. Wet snow may clog the gauge and cause underreporting
while dry snow frequently will be blown out of the gauge, also causing
underestimation of precipitation. The gauge selected has a 30 cm diameter
orifice and generates a bucket tip for every 0.25 mm of rain. The counts
are accumulated over a 5-minute interval. It was necessary to locate the
rain gauge close to the 10 meter tower and the tower location was selected
to optimize wind fetch. The top of the gauge is 0.6 m above ground level.
Since the largest source of rain gauge error, after sampling error, is
due to wind induced precipitation loss, an Alter-style wind screen is used
to reduce the wind effect.

Data sampling and averaging are performed at two levels
in the ASOS, at the sensor level and at the ACU level
as shown in Table 8.4. For example, the temperature and dew point are sampled
at 30 s intervals and 1 minute averages are generated at the sensor level.
Then the ACU algorithms take the 1-minute averages, perform some quality
assurance checks (see below) and generate 5-minute averages which are updated
every minute. The 5-minute average is reported every minute in the OMO
and the most recent 5-minute average is reported in the SAO.
|
|
|
|
|||
|
|
|
|
|
|
|
| Cloud height | 1.3 ms | 12 s | 30 s | 30 min | 1 min |
| Visibility | 30 s | 1 min | 1 min | 10 min | 1 min |
| Present weather | 1 s | 1 min | 1 min | 10 min | 1 min |
| Freezing rain | 1 s | 1 min | 1 min | 15 min | 1 min |
| Temp. & dew point | 30 s | 1 min | 1 min | 5 min | 1 min |
| Wind | 1 s | 5 s | 5 s | 2 min | 1 min |
| Pressure | 10 s | 1 min | 1 min | 1 min | 1 min |
| Precipitation | 1 s | 1 min | 1 min | 15 min,
1 hr |
15 min,
1 hr |
Wind speed and direction are sampled at 1 s intervals at the sensor level in the ASOS where 5 s averages are formed. At the ACU level, the 5 s averages are further averaged over 2 minutes which are updated every 5 s. The ASOS reports wind character as gusts, squalls, variable wind direction, wind shift, peak wind, daily peak wind, and fastest 2-minute wind. A simplified version of the wind gust definition is that a gust is the maximum 5-s average observed over the last 10 minutes if that gust is greater than 7 m/s and the 2-minute average is greater than 1 m/s . ASOS does not perform vector averages nor does it compute standard deviations of wind variables.
Local data processing capability in the PAM is intermediate between the ASOS and the Mesonet. PAM has a more powerful processor and is easier to program.
The data logger, located in each remote station, is the heart of the measurement system since all data flow through it. The Mesonet uses Campbell Scientific CR1 OT data loggers. They perform analog to digital conversion, on-site data processing and play an essential role in the digital data communications link. The logger also limits the number of sensors of each type (up to 12 analog, two event or counter, and eight digital input-output lines) that can be installed at a given site. (It is possible to install more analog sensors by adding a multiplexer expansion module.)
The analog subsystem accommodates the sensors whose output is a voltage signal and those whose output can be readily converted to a voltage. These include the wind vane, the air and soil temperature sensors, the relative humidity sensor and the pyranometer.
A digital input-output port (or line) can be used with a tipping-bucket rain gauge by programming the data logger to enter a subroutine each time the port senses a low-to-high transition. The subroutine counts the number of times it has been entered and, therefore, the number of tips of the bucket. These ports control the barometer, which has its own microprocessor, and to read the serial digital signal.
The data logger provides sufficient programming capability to perform the local processing: setting the sampling and averaging periods, determining which input channels are to be read and how they are to be processed, and what data are to be output and in what order. Local memory is used to store the operating program, and to provide temporary storage of intermediate operands and of data waiting for transmission. In the Mesonet configuration, the data logger has sufficient memory to store data for a week without loss in the event of a communications failure.
Each Mesonet remote station generates a data message every
15 minutes. Each message is a composite of three 5-minute averages of most
variables and a 15-minute average of the remaining variables as indicated
in Table 8.5. In addition, some housekeeping variables are reported such
as the battery voltage.
|
|
|
|
|
| Wind speed 10 m | Count 3s | 5 min | Wind run (scalar average)
Wind speed (vector average) Wind direction (vector average) Wind direction standard deviation Wind speed standard deviation Wind speed maximum |
| Wind direction 10 m | 3 s | 5 min | |
| Air temperature
1.5 m and 9 s (S) |
3 s | 5 min | Average |
| Relative Humidity 1.5 m | 3 s | 5 min | Average |
| Barometric Pressure | 12 s | 5 min | Average |
| Rainfall | -- | 5 min | Accumulative rainfall |
| Solar Radiation | 3 s | 5 min | Average |
| Wind speed 2 m (S) | 3 s | 5 min | Average |
| Soil temperatures | 30 s | 15 min | Average |
| Leaf wetness (S) | 30 s | 15 min | Average |
Wind direction is sampled every 3 s while wind speed is counted or integrated over a 3-second period. Thus there are 100 samples of wind speed and direction in each 5-minute averaging period. The maximum wind speed is defined to be the maximum 3-second speed within a 5-minute period. Wind speed max is not comparable to the ASOS wind gust. Wind run is the scalar average of the wind speed. Wind speed and direction are the vector average of the speed and direction. Standard deviations of the speed and direction are taken over the scalar quantities.
Power to the barometer is turned on only during a measurement. It takes the barometer 1 s to stabilize and generate a reading after the power is turned on. In the Mesonet, the barometers are sampled at 12 s intervals. They are turned on and allowed to stabilize for 3 s, then the pressure is read and the barometer is turned off. The power duty cycle is approximately 0.25.
Rainfall is the count of bucket tips over the averaging
period. Pulses from the 2 m wind speed anemometer, like the 10 m wind speed
propeller, are counted over the averaging period. Sample averages for the
other variables in Table 8.3 are scalar averages of the instantaneous readings
taken at the sampling period (3 s or 30 s) during the averaging period.
At the regional level, the ASOS messages are checked for error indicators and technicians are dispatched as needed to the individual sites. There are no technicians permanently resident at the local level so all maintenance comes from the regional level.
Messages are checked at the national level to determine whether they arrive within an allotted time window. This central facility synchronizes clocks at all the ASOS stations and maintains data such as station elevation and magnetic declination. At the National Meteorological Center (NMC) the data are checked for consistency with the NMC optimal interpolation analysis. The National Climatic Data Center (NCDC) may perform additional quality control of the ASOS data before they are archived. This last check would not be done in real time so could not be used for the usual maintenance but would serve as a long term check on performance.
The objective of the data quality assurance (QA) program is to maintain the highest possible data quality in a network (Brock and Fredrickson, 1993). To achieve this goal, data faults must be detected rapidly, corrective action must be initiated in a timely manner, and questionable data must be flagged. The data archive must include provision for status bits associated with each datum. The QA system is designed to never alter the data but only to set status bits that indicate the probable data quality. It is possible the QA system will flag data that actually is valid but represents unusual or unexpected meteorological conditions; with this QA system, the actual reported data always will be available. In addition, flagged data will be available to some users but will not be available for routine operational use.
The major components required for this program are laboratory
calibrations, field intercomparisons, real-time monitoring of the data,
documentation, independent reviews, and publication of data quality assessment.
There are two types of field intercomparisons that must be done. The Mesonet has a field intercomparison station located near Norman. And when technicians visit a Mesonet station, they carry portable transfer standards and make a routine comparison check.
1) Field Intercomparison Station
The field intercomparison station is a special remote station, referred to as a reference station and equipped with better sensors, that is located adjacent to a standard station. Two Mesonet stations are collocated with ASOS stations. These stations are used for intercomparison to provide an on-going check of sensor performance in the field. In addition, the reference station can be used to test proposed new sensors.
2) Routine Intercomparisons
Several sets of portable transfer sensors are available;
each time a technician visits a station, reference measurements are made.
This can be used to detect drift or other failures of sensors that might
otherwise go undetected. These sensors can be standard sensors that have
been carefully calibrated and checked frequently to insure against drift.
Technicians carry a lap-top computer to read current data and to read the
portable reference instruments. Some problems can be detected in the field.
Regardless, the usual fix is to replace sensors or modules and not attempt
repairs in the field. Routine visits for preventative maintenance will
be scheduled at intervals of three months. Real-time, automatic monitoring
of the data, described below, will detect many problems and other visits
to stations will be scheduled as needed.
Some elements of the QA system are fairly simple and can be used to test each datum as it arrives in the central computer. The range test, as used by the ASOS, is an example of a very simple but quite effective algorithm. Other tests are run periodically as sufficient data accumulates - these use time series or time series in conjunction with spatial analysis.
In general, the QA programs utilize knowledge of the instrumentation
system, knowledge of the atmosphere and statistical techniques.
An instrumentation data base should contain sensor serial
number, current location of the sensors, and the operational status. Some
sensors have individual calibration coefficients so there must be a method
of accounting for sensors to insure that the correct calibration coefficients
have been entered.
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