BOREAS RSS-12 Airborne Tracking Sunphotometer Measurements

Summary

The BOREAS RSS-12 team collected both ground and airborne sunphotometer 
measurements for use in characterizing the aerosol optical properties of the 
atmosphere during the BOREAS data collection activities. These measurements are 
to be used to: 1) measure the magnitude and variability of the aerosol optical 
depth in both time and space; 2) determine the optical properties of the boreal 
aerosols; and 3) atmospherically correct remotely sensed data acquired during 
BOREAS. This data set contains airborne tracking sunphotometer data that were 
acquired from the C-130 aircraft during its flights over the BOREAS study areas. 
The data cover selected days and times from May to September 1994. The data are 
stored in tabular ASCII files.

Table of Contents

   *  1 Data Set Overview
   *  2 Investigator(s)
   *  3 Theory of Measurements
   *  4 Equipment
   *  5 Data Acquisition Methods
   *  6 Observations
   *  7 Data Description
   *  8 Data Organization
   *  9 Data Manipulations
   *  10 Errors
   *  11 Notes
   *  12 Application of the Data Set
   *  13 Future Modifications and Plans
   *  14 Software
   *  15 Data Access
   *  16 Output Products and Availability
   *  17 References
   *  18 Glossary of Terms
   *  19 List of Acronyms
   *  20 Document Information

1. Data Set Overview

1.1 Data Set Identification

BOREAS RSS-12 Airborne Tracking Sunphotometer Measurements

1.2 Data Set Introduction

The Airborne Tracking Sunphotometer (ATSP) data set consists of instrument 
voltages; Sun position information; ozone (O3), nitrogen dioxide (NO2) and 
aerosol optical depth values.  These data were collected and processed by the 
BOReal Ecosystem-Atmosphere Study (BOREAS) Remote Sensing Science Team 12 (RSS-
12) at the National Aeronautics and Space Administration (NASA) Ames Research 
Center (ARC).  The data provide a good characterization of atmospheric aerosols 
during the C-130 flights.

1.3 Objective/Purpose

The overall goal of this investigation was to measure aerosol optical properties 
from both ground- and aircraft-based sunphotometers during the 1994 BOREAS 
Intensive Field Campaigns (IFCs). These measurements are to be used to:

   1) Measure the magnitude and variability of the aerosol optical 
      depth in both time and space. 
   2) Determine the optical properties of the boreal aerosols.
   3) Atmospherically correct selected remotely sensed data acquired 
      during BOREAS. 

1.4 Summary of Parameters

The phenomenon being measured is the atmospheric aerosol optical depth. The 
parameters include Rayleigh optical depth, aerosol optical depth, time, 
latitude, longitude, air mass, solar position, and aircraft altitude.

1.5 Discussion

The ATSP data were used in conjunction with the Automated Ground Sunphotometer 
(AGSP) data to determine the magnitude and variability of the aerosol optical 
depth in both time and space.  The aerosol optical depth data will be inverted  
using an algorithm developed by King et al., 1978, to derive the size 
distribution of the boreal aerosols. Mie theory will then be used to calculate 
the aerosol phase function and single-scattering albedo. Finally, the 
atmospheric correction algorithm of Wrigley et al., 1992 will be used to 
atmospherically correct selected NS001 Thematic Mapper Simulation (TMS), Landsat 
Thematic Mapper (TM), and MODerate-resolution Imaging Spectrometer (MODIS) 
Airborne Simulator (MAS) data collected during the 1994 BOREAS IFC's.

Atmospheric correction of Landsat TM and other satellite data will use the 
aerosol properties derived from surface optical depth measurements. Atmospheric 
correction of NS001 and MAS data will use aerosol properties derived from the 
airborne optical depth measurements as well as those from the surface 
measurements.

1.6 Related Data Sets

BOREAS RSS-12 Automatic Ground Sunphotometer Measurements in the SSA
BOREAS RSS-11 Ground Network of Sunphotometer Measurements 
BOREAS RSS-18 Ground Sunphotometer Measurements in the SSA

2. Investigator(s)

2.1 Investigator(s) Name and Title

Robert C. Wrigley (retired 1995)
Principal Investigator

Co-Investigators:

Michael A. Spanner             
Robert E. Slye  
Philip B. Russell           
John M. Livingston


2.2 Title of Investigation

Aerosol Determinations and Atmospheric Correction for BOREAS Imagery

2.3 Contact Information

Contact 1
--------------------------------
Michael A. Spanner
Co-Investigator
Johnson Controls World Services
NASA Ames Research Center
Moffett Field, CA 
(415)604-3620
mspanner@gaia.arc.nasa.gov

Contact 2
-------------------------------
Jaime Nickeson
NASA/GSFC
Greenbelt, MD 
(301) 286-3373
(301)286-0239(fax)
Jaime.Nickeson@gsfc.nasa.gov


3. Theory of Measurements

The ATSP measures direct-beam solar radiation for six channels in the visible 
and near-infrared wavelengths. The solar radiation data are collected in the 
form of voltages. The instrument was calibrated before and after the experiment 
at high mountain observatories, which often have clean, stable air masses, so 
the Langley plot technique could be used. For calibration, data are collected at 
a range of solar angles from low solar elevation (air mass=5) to high solar 
elevation (air mass =1.8). A regression is developed between log voltage and air 
mass. This regression equation is then extrapolated to an air mass of 0. This 
value called the zero air mass intercept voltage, is the value used to calibrate 
the instrument in a given channel. Great care must be taken to ensure the 
stability of these intercept voltages over time. A calibration history is 
maintained that attests to the stability of the instrument. The voltages 
measured by the instrument during the BOREAS IFCs were converted to total 
optical depth using the zero air mass intercept voltages calculated from the 
calibrations using the equation:

V/Vo = (Rm/R)^2 exp(-mt)

where V is the measured voltage, Vo is the zero air mass voltage intercept, R is 
the radius of Earth's orbit at the time, Rm is the mean radius, m is the air 
mass at the time, and t is the total optical depth (usually written as  the 
Greek letter tau). The aerosol optical depth is calculated from the total 
optical depth by subtracting a number of components that contribute to the total 
optical depth: Rayleigh scattering and gaseous absorption due to ozone and NO2. 
The Rayleigh optical depth is calculated using pressure measured on the 
aircraft. NO2and ozone optical depths are subtracted from the total minus 
Rayleigh optical depth to obtain the aerosol optical depth. NO2 abundance is 
obtained from climatology tables based on Noxon, 1979, and convolved with 
absorption coefficients at ATSP wavelengths. Ozone optical depth is calculated 
using ozone abundances from the Total Ozone Mapping Spectrometer (TOMS) 
satellite instrument and convolved with absorption coefficients at ATSP 
wavelengths. The result of this processing is the aerosol optical depth measured 
in five channels (not including the 940 nm water vapor channel) at approximately 
2-second intervals in the air and 10 second intervals on the ground. 

The correction of remote sensing data acquired from satellites or aircraft for 
effects due to the intervening atmosphere has proven to be a difficult problem. 
Not only does the atmosphere reduce the transmission of the incoming, reflected, 
and emitted radiation, but it contributes reflected and emitted radiation of its 
own. Under high aerosol concentration conditions, atmospheric radiation 
comprises over 90% of the satellite-observed radiance, but even much smaller 
effects would degrade the quantitative use of these data unless they are taken 
into account. The interaction of radiation with the atmosphere is complex and 
has proved difficult to calculate without reference to measurements made at, or 
close to, the time and location of interest. Effects due to Rayleigh scattering 
from atmospheric gases are well understood because the major gases (nitrogen, 
oxygen) that comprise 99% of the atmosphere are well mixed and their 
concentrations with altitude are known. The effects because of small particle 
(aerosol) scattering are quite variable because of the wide range of aerosol 
concentrations; and the variety of aerosols found in the atmosphere. Because 
aerosol concentrations cannot be known a priori, they must be measured at the 
time and location of remote sensing data acquisition.

The physical properties of aerosols such as size, shape, refractive index, and 
concentration in the atmosphere control the aerosol interaction with light 
according to a set of optical properties. Three fundamental properties are (1) 
the aerosol optical depth, an indirect measure of the size and number of 
particles present in a given column of air; (2) the single scattering albedo; 
the fraction of light intercepted and scattered by a single particle; and (3) 
the phase function; a measure of the light scattered by a particle as a function 
of angle with respect to the original direction of propagation.

4. Equipment

4.1 Sensor/Instrument Description

The instrument consists of a solar-tracking system, detector module, temperature 
control system, nitrogen-purge system, mechanical drive chain, and data 
collection system.

4.1.1 Collection Environment

The ATSP was used for data collection while mounted on the NASA C-130 aircraft. 
Data were collected while the aircraft was on the ground and during flight at 
altitudes up to 10,120 meters.

4.1.2 Source/Platform

The ATSP was mounted on the NASA ARC C-130 Earth Resources aircraft.

4.1.3 Source/Platform Mission Objectives

The ATSP was developed to obtain accurate multispectral atmospheric extinction 
measurements at different altitudes. 

4.1.4 Key Variables

The primary quantity being measured is the total optical depth. The aerosol 
optical depth is derived by subtracting optical depths caused by other 
components of the atmosphere: Rayleigh scattering, ozone absorption, and NO2 
absorption.

4.1.5 Principles of Operation

The sensors used are Clairex photoresistors that have been matched to track each 
other over the operational range of Sun intensities. The sensing technique uses 
a shadow mask that bisects each detector when the system is in balance. The 
design allows for very accurate tracking, yet at the same time provides a Field-
of-View (FOV) and accurate tracking in a very compact package. The dome rotation 
is referred to as azimuth motion. The central section of the dome is free to 
rotate within the dome, perpendicular to the azimuth, and is referred to as 
elevation motion. The control system is designed to compensate for the flight 
characteristics of the aircraft.

4.1.6 Sensor/Instrument Measurement Geometry

The six separate detectors view the Sun simultaneously at six independent 
wavelengths. The FOV of each detector is set by the entrance aperture to 4 
degrees; the inside surfaces of the aperture assembly are anodized a dull black 
to reduce internal reflections. The 4-degree FOV was selected to allow for +/-1 
degree of tracking error without affecting the solar-radiation signal. The 
wavelengths and the full width half maximum (FWHM) of the ATSP are shown in the 
following table for all channels.

 Wavelength (nm)  FWHM (nm)
 ---------------  ---------
     379.8          11.0
     451.3           6.2
     525.7           9.1
     860.5          13.0
     940.0           0.2
    1059.9          12.7

The system is designed to move in elevation or azimuth at 8 degrees per second. 
The acceleration that may occur during a turn is estimated to be 1.0 radian per 
second squared. If the instrument should lose lock, the reacquisition occurs 
very rapidly as long as the Sun is in the FOV of the instrument. The tracking 
system responds quickly because it uses a single rate of 8 degrees per second 
for tracking. The solar-tracking system was designed to achieve two objectives: 
first, to be able to acquire the Sun starting from a position several degrees 
away; and second, to track the Sun with an accuracy of +/-2 degrees in the 
presence of aircraft movements.

4.1.7 Manufacturer of Sensor/Instrument

Manufactured by NASA ARC, Moffett Field, CA 94035, Dr. Philip Russell, Principal 
Investigator.

4.2 Calibration

4.2.1 Specifications

The detectors are temperature controlled, and the amplifier gains are set with 
precision resistors. The resolution of the detector signals is limited by the 
12-bit analog-to-digital converter that can resolve 1 part out of 2048 of the 0 
to +10v detector signals. The instrument is designed to operate in clear skies, 
and it is assumed that over the period of a flight profile, there are no solar 
fluctuations. 

4.2.1.1 Tolerance

There is evidence in the literature that in the wavelength region of interest, 
solar fluctuations would account for less than a 1% variation of the data.

4.2.2 Frequency of Calibration

The instrument was calibrated at the Mt. Lemmon Steward Observatory, Tucson, AZ, 
in April 1994 (before the field season) and at the Mauna Loa Observatory, HI in 
November 1994 (after the field season).

4.2.3 Other Calibration Information

The calibration coefficients, corrected for Earth-Sun distance, are contained in 
the data files.

5. Data Acquisition Methods

The data collection system was based on a Hewlett-Packard HP9816 computer with 
floppy disk and printer. This system was used to run data collection, data 
processing, and printing software developed by NASA ARC. In addition to the 
computer, the data collection system included a multiplexer, a 12-bit analog-to 
-digital converter, and electronics to process the aircraft inertial navigation 
data. The data are sampled approximately every 2-seconds and are synchronized 
with the aircraft data system, which provides the altitude, longitude, and 
latitude data. The science data set includes the six detector signals, detector 
temperature, tracking error, Sun tracker azimuth angle, Sun tracker elevation 
angle, and Universal Time Code (UTC) time. The data were stored on 3.5-inch 
floppy disks and were also printed for real-time check and backup. Data were 
collected for the duration of the optical flights of the C-130 aircraft and were 
collected on the ground before and/or after the flights to determine the total 
atmospheric aerosol optical depth.

A new data collection system is under design and construction. It will be based 
on a 486 laptop PC running Visual Basic in a Windows environment. Digital-to -
analog conversion will be significantly enhanced and optimized for each channel 
using a Dacbook. Data reduction will be simplified because the necessity for 
hex-to-ASCII conversion will be eliminated. Several programs currently requiring 
processing on minicomputers will be installed on the PC; this will permit 
processing to semifinal products in the field (only the postmission calibration 
will have to be incorporated into the final products).

6. Observations

6.1 Data Notes

Below is a table of 

SPATIAL_COVERAGE     C130_SITE C130_LINE_NUM
-------------------- --------- -------------
SSA                     429                  0
SSA-LAKE                429                  9
SSA-LAKE                429                 10
SSA-OBS                 429                101
SSA-OBS                 429                102
SSA-OBS                 429                103
SSA-OJP                 429                201
SSA-OJP                 429                202
SSA-OJP                 429                203
SSA-9OA                 429                301
SSA-9OA                 429                302
SSA-9OA                 429                303
SSA-YJP                 429                401
SSA-YJP                 429                402
SSA-YJP                 429                403
SSA-9YA                 429                501
SSA-9YA                 429                502
SSA-9YA                 429                503
SSA-CAL                 429                601
SSA-CAL                 429                603
SSA-FEN                 429                701
SSA-FEN                 429                702
SSA-FEN                 429                703
SSA                     430                  0
SSA-MSA                 430                  1
SSA-MSA                 430                  2
SSA-MSA                 430                  3
SSA-MSA                 430                  4
SSA-MSA                 430                  5
SSA-MSA                 430                  6
SSA-MSA                 430                  7
SSA-MSA                 430                  8
SSA-MSA                 430                  9
SSA-MSA                 430                 10
SSA-MSA                 430                 11
NSA                     431                  0
CALIB_FROZEN_LAKE    KE 431                  1
NSA-OBS                 431                101
NSA-OBS                 431                102
NSA-OBS                 431                103
NSA-FEN                 431                201
NSA-FEN                 431                202
NSA-FEN                 431                203
NSA-OJP                 431                301
NSA-OJP                 431                302
NSA-OJP                 431                303
NSA-YJP                 431                401
NSA-YJP                 431                402
NSA-YJP                 431                403
NSA-9OA                 431                601
NSA-9OA                 431                602
NSA-9OA                 431                603
NSA                     432                  0
NSA-MSA                 432                  1
NSA-MSA                 432                  2
NSA-MSA                 432                  3
NSA-MSA                 432                  4
NSA-MSA                 432                  5
NSA-MSA                 432                  6
NSA-MSA                 432                  7
NSA-MSA                 432                  8
NSA-MSA                 432                  9
TRANSECT                433                  0
TRANSECT                433                  1
TRANSECT                433                  2
TRANSECT                433                  3
TRANSECT                433                  4
TRANSECT                433                  5
NSA-MSA                 999                999
NSA                     BTW                  0
SSA                     BTW                  0
NSA                     DSC                  0
SSA                     DSC                  0
TRANSECT                DSC                  0
NSA                     PRE                  0
SSA                     PRE                  0
TRANSECT                PRE                  0
TRANSECT                TRN                  0
SSA                     YPA                  0
NSA                     YTH                  0

6.2 Field Notes

The ATSP operator normally takes notes of significant events while the 
instrument is acquiring data. These notes supplement the real-time display of 
detector voltages or optical depths and permit determination of the presence of 
variable cloud interference with remote sensing data collection; this feature 
often indicates whether or not a given flight line was acceptable or had to be 
repeated. If the line was acceptable, then the notes, if any, help identify data 
problems during processing.  Anyone interested in these notes should contact 
RSS-12 personnel at NASA ARC.

7. Data Description

7.1 Spatial Characteristics

The ATSP views the Sun with a 4-degree FOV and typically acquires data every 2 
or 3 seconds during flight. A typical ground speed of the C-130 aircraft is 150 
m/sec. Hence, data are collected every 300 meters along a flight line. During 
spiral descents and ascents, typical vertical rates are 1,000 ft/min or 5 m/sec 
so the ATSP samples the vertical column every 10 meters.

7.1.1 Spatial Coverage

Although most of the data were collected over the BOREAS Northern Study Area 
(NSA), Southern Study Area (SSA), and tower sites, some data are available over 
the transect between the NSA and SSA.

The North American Datum 1983 (NAD83) corner coordinates of the 1,000- by 
1,000- km BOREAS region are: 

           Latitude     Longitude
          ----------   -----------
Northwest 59.97907 N   111.00000 W
Northeast 58.84379 N    93.50224 W
Southwest 51.00000 N   111.00000 W
Southeast 50.08913 N    96.96951 W


The NAD83 corner coordinates of the NSA are:

            Latitude     Longitude
            --------     ---------
Northwest    56.249 N      98.825 W
Northeast    56.083 N      97.234 W
Southwest    55.542 N      99.045 W
Southeast    55.379 N      97.489 W

The NAD83 corner coordinates of the SSA are:

             Latitude     Longitude
             --------     ---------
Northwest    54.321 N     106.228 W
Northeast    54.225 N     104.237 W
Southwest    53.515 N     106.321 W
Southeast    53.420 N     104.368 W


7.1.2 Spatial Coverage Map

Not available.

7.1.3 Spatial Resolution

The sunphotometer's spatial resolution was variable based on aircraft maneuvers 
and flight speed. If the sunphotometer was acquiring data every 2-seconds and 
the C-130 was flying level at 150 m/sec, then the ground resolution was 300 
meters.

7.1.4 Projection

The coordinates in the data files are from the C-130 internal navigation system 
(INS). The INS geographic position data are from the onboard Global Positioning 
System (GPS), which uses NAD83.

7.1.5 Grid Description

Not applicable.

7.2 Temporal Characteristics

7.2.1 Temporal Coverage

Data were acquired during three IFCs in 1994. The days and times were:

Date         Time (GMT)       
-----------  -----------------
25-May-1994  15:21:28-18:02:23
26-May-1994  12:51:41-19:15:20
31-May-1994  13:30:20-16:30:26
01-Jun-1994  13:34:43-15:20:41
04-Jun-1994  13:08:07-18:53:02
06-Jun-1994  15:07:25-17:33:26
07-Jun-1994  14:15:28-17:08:53
08-Jun-1994  14:04:34-22:29:33
20-Jul-1994  15:12:04-18:25:55
21-Jul-1994  13:46:30-17:33:00
22-Jul-1994  14:04:43-17:27:18
23-Jul-1994  13:44:38-14:41:09
24-Jul-1994  13:50:45-14:08:24
26-Jul-1994  16:08:00-17:15:44
29-Jul-1994  13:21:03-18:16:19
31-Jul-1994  12:59:18-18:24:25
02-Aug-1994  13:09:15-18:07:19
03-Aug-1994  14:37:00-16:46:39
04-Aug-1994  12:45:25-22:23:19
08-Aug-1994  12:47:45-15:43:01
09-Aug-1994  12:36:04-19:20:08
10-Aug-1994  13:21:34-18:08:37
31-Aug-1994  14:05:24-19:55:39
01-Sep-1994  00:40:38-14:27:32
02-Sep-1994  13:51:45-17:10:32
03-Sep-1994  14:08:56-16:53:50
06-Sep-1994  15:03:13-18:33:01
08-Sep-1994  14:02:31-17:41:14
09-Sep-1994  15:49:51-16:00:32

7.2.2 Temporal Coverage Map

Not available.

7.2.3 Temporal Resolution

The ATSP typically samples every 2 or 3 seconds during flight, but the sampling 
rate is under computer control and can be modified if necessary. 

7.3 Data Characteristics

Data characteristics are defined in the companion data definition file 
(sunphair.def).


7.4 Sample Data Record

Sample data format shown in the companion data definition file (sunphair.def).

8. Data Organization

8.1 Data Granularity

All of the Airborne Tracking Sunphotometer Measurement Data are contained in one 
file.

8.2 Data Format(s)

The data file contains numerical and character fields of varying length 
separated by commas. The character fields are enclosed with single apostrophe 
marks. There are no spaces between the fields. Sample data records are shown in 
the companion data definition files (sunphair.def).

9. Data Manipulations

9.1 Formulae

For all sunphotometer channels except the 940 nm, the Bouguer-Lambert-Beer 
extinction law was used to describe the attenuation of solar radiation:

V = (R'/R)^2 V0 exp(-m tau) = V'0 exp(-m tau)

where V is the output voltage of the detector at a given wavelength, V0 is the 
zero air-mass voltage intercept at that wavelength for the mean Earth-Sun 
separation R', R is the Earth-Sun separation at the time of observation, m is 
the atmospheric air mass between the instrument and the Sun, tau is the 
wavelength-dependent total vertical optical depth above the sunphotometer, and 
V'0 is the zero-air-mass voltage intercept for the Earth-Sun separation R at the 
time of observation. The 940-nm channel requires different processing and is not 
included this data set.

The logarithm of the above equation,

ln V = ln V'0 - m tau,

is used in calibration to provide the V'0 values for each channel (i.e., zero 
air mass Langley plot intercept voltages). When the detector voltages are 
plotted against the air mass, the intercept is the V'0. After calibration, this 
equation can be solved for tau to provide the total optical depth. The total 
optical depth is then decomposed using 

tau = tau_r + tau_a + tau_O3 + tau_NO2 + tau_H2O,

where these terms are the optical depth due to Rayleigh scattering, aerosols, 
ozone, NO2, and water vapor, respectively. The source for each of these terms is 
given in Section 7.3. Water vapor was ignored because it contributes in the 940- 
nm channel.

This description is taken from Spanner et al., 1990, where more information 
concerning the data processing can be found.

9.1.1 Derivation Techniques and Algorithms

A description of algorithms can be found in Spanner et al., 1990.

9.2 Data Processing Sequence

9.2.1 Processing Steps

The steps for processing are as follows: 1) acquire the data; 2) run a program 
to calculate all the variables, including solar zenith angle, air mass, Rayleigh 
optical depth, and instantaneous optical depth (total optical depth minus 
Rayleigh optical depth); 3) calculate NO2 and ozone optical depths from Noxon et 
al., 1979, and TOMS data, respectively; and 4) subtract NO2 and ozone to derive 
aerosol optical depth.
 
The ozone abundance was determined from the TOMS satellite instrument convolved 
with ozone absorption coefficients from Penney (1979). The values calculated for 
NO2 and ozone optical depth were subtracted from the instantaneous optical depth 
to derive the aerosol optical depth, are provided in the data files.

9.2.2 Processing Changes

None given.

9.3 Calculations

9.3.1 Special Corrections/Adjustments

No special corrections or adjustments have been made.

9.3.2 Calculated Variables

Description of algorithms can be found in Spanner et al., 1990.

9.4 Graphs and Plots

Plots have been provided to BORIS and can be made available upon request.

10. Errors

10.1 Sources of Error

Calibration errors are the main source of error in the derivation of aerosol 
optical depth.

10.2 Quality Assessment

10.2.1 Data Validation by Source

Data were compared with the RSS-11 field sunphotometer (see related data sets, 
Section 1.6).

10.2.2 Confidence Level/Accuracy Judgment

The data are of high quality, because a good calibration of the instrument was 
performed before and after the BOREAS field collection effort. 

10.2.3 Measurement Error for Parameters

Uncertainties for the aerosol optical depths were determined by using 
uncertainty propagation through the algorithm. The aerosol optical depth 
uncertainty is dependent on the uncertainty in the Rayleigh, ozone, and 
NO2optical depths, as well as the uncertainty in the intercept voltage 
(calibration error), instantaneous measurement, and airmass. Aerosol optical 
depth uncertainties are given in the data files and are summarized in Section 
7.3 of this document.

10.2.4 Additional Quality Assessments

None.

10.2.5 Data Verification by Data Center

Visual review and use of selected subsets of the data have shown them to be of 
good quality with no noteworthy problems.

11. Notes

11.1 Limitations of the Data

None.

11.2 Known Problems with the Data

None.

11.3 Usage Guidance

The values of aerosol optical depth are accurate instantaneous values of aerosol 
optical depth. These data were taken frequently; therefore, under conditions of 
rapid variability in cloudiness or haze, the data may not be internally 
consistent or appropriate. It is useful to calculate averages of aerosol optical 
depth over periods of time to get a more accurate measure of the average 
conditions at a site.

Users should take note that the daily extrated files have a large size range 
(400 to 38,000 records)

11.4 Other Relevant Information

The aerosol optical depth at 941 nm was not calculated because this channel 
primarily measures absorption due to water vapor.

12. Application of the Data Set

These data can be used for correcting various visible and infrared satellite and 
aircraft image products or for characterizing the atmospheric aerosols at the 
times of the flights.

13. Future Modifications and Plans

Future plans for the airborne instrument include the design and development of a 
new 14-channel airborne instrument.

14. Software

14.1 Software Description

NASA ARC software was developed in FORTRAN on a VAX to implement the data 
processing procedure described in Section 9.1. Input data include sunphotometer 
data files as well as ozone and NO2 optical depth parameters. Aerosol optical 
depths were calculated and written to the data files. No special software is 
needed to read the data files because they are stored comma delimited.

14.2 Software Access

This software is used to generate the data product from the detector voltages 
and is not needed to use the data.

15. Data Access

15.1 Contact Information

Ms. BethNelson
BOREAS Data Manager
NASA GSFC
Greenbelt, MD 
(301) 286-4005
(301) 286-0239 (fax)
beth@ltpmail.gsfc.nasa.gov

15.2 Data Center Identification

See Section 15.1.

15.3 Procedures for Obtaining Data

Users may place requests by telephone, electronic mail, or fax.

15.4 Data Center Status/Plans

The RSS-12 C130 sunphotometer data are available from the Earth Observing System 
Data and Information System (EOSDIS) Oak Ridge National Laboratory (ORNL) 
Distributed Active Archive Center(DAAC). The BOREAS contact at ORNL is: 

ORNL DAAC User Services
Oak Ridge National Laboratory
Oak Ridge, TN 
(423) 241-3952
ornldaac@ornl.gov
ornl@eos.nasa.gov

16. Output Products and Availability

16.1 Tape Products

None.

16.2 Film Products

None.

16.3 Other Products

The data are available as tabular ASCII files.

17. References

17.1 Platform/Sensor/Instrument/Data Processing Documentation

None.

17.2 Journal Articles and Study Reports

Bruegge, C.J., R.N. Halthore, B. Markham, M. Spanner, and R. Wrigley. 1992. 
Aerosol optical depth retrievals over the Konza prairie. Journal of Geophysical 
Research 97(D17):18743-18758.

King, M., D. Bryne, B. Herman, and J. Reagan. 1978. Aerosol size distributions 
obtained by inversion of spectral optical depth measurements. J. Atmos. Sci. 
35:2153-2167.

Noxon, J. 1979. Stratospheric NO2, 2, Global behavior, J. Geophys. Res. 84:5067-
5076.

Penney, C.M. 1979. Study of temperature dependence of the Chappuis band 
absorption of ozone, NASA Contract Rep. 158977, General Electric  Company, 
Schenectady, N.Y.

Russell, P., J. Livingston, E. Dutton, R. Pueschel, J. Reagan, T. DeFoor, M. 
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and pre-Pinatubo optical depth spectra:  Mauna Loa measurements, comparisons, 
inferred particle size distributions, radiative effects, and relationship to 
lidar data. J. Geophys. Res. 98:22,969-22,985.

Sellers, P.and F. Hall. 1994. Boreal Ecosystem-Atmosphere Study: Experiment 
Plan. Version 1994-3.0, NASA BOREAS Report (EXPLAN 94). 

Sellers, P.and F. Hall. 1996. Boreal Ecosystem-Atmosphere Study: Experiment 
Plan. Version 1996-2.0, NASA BOREAS Report (EXPLAN 96). 

Sellers, P.and F. Hall and K.F. Huemmrich. 1996. Boreal Ecosystem-Atmosphere 
Study: 1994 Operations. NASA BOREAS Report (OPS DOC 94). 

Sellers, P., F. Hall and K.F. Huemmrich. 1997. Boreal Ecosystem-Atmosphere 
Study: 1996 Operations. NASA BOREAS Report (OPS DOC 96). 

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Cihlar, M.G. Ryan, B. Goodison, P. Crill, K.J.Ranson, D. Lettenmaier, and D.E. 
Wickland. 1995. The boreal ecosystem-atmosphere study (BOREAS): an overview and 
early results from the 1994 field year. Bulletin of the American Meteorological 
Society. 76(9):1549-1577. 

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17.3 Archive/DBMS Usage Documentation

18. Glossary of Terms

air mass       - secant of the solar zenith angle

optical depth  - an indirect measure of the size and number of 
                 particles present in a given column of air, which is a 
                 measure of the extinction of the direct solar beam by 
                 aerosols and particulates in the atmosphere, or by 
                 scattering.  Also referred to as optical thickness.

phase function - a measure of the light scattered by a particle as a 
                 function of angle with respect to the original 
                 direction of propagation

radiometer     - an instrument for measuring radiant energy

Rayleigh       - wavelength-dependent scattering directly proportional
scattering       to (1 + cos2(angle)) and indirectly proportional to 
                 wavelength4

single         - the fraction of light intercepted and scattered by a
scattering       single particle
albedo

19. List of Acronyms

 AGSP    - Automated Ground Sunphotometer
 ARC     - Ames Research Center
 ATSP    - Airborne Tracking Sunphotometer
 BOREAS  - BOReal Ecosystem-Atmosphere Study
 BORIS   - BOReas Information System
 DAAC    - Distributed Active Archive Center
 EOS     - Earth Observing System
 EOSDIS  - EOS Data and Information System
 FIFE    - First ISLSCP Field Experiment
 FOV     - Field-of-View
 FWHM    - Full Width Half Maximum
 GMT     - Greenwich Mean Time
 GPS     - Global Positioning System
 GSFC    - Goddard Space Flight Center
 IFC     - Intensive Field Campaign
 INS     - Inertial Navigation System
 ISLSCP  - International Satellite Land Surface Climatology Project
 MAS     - MODIS Airborne Simulator
 MODIS   - MODerate-resolution Imaging Spectrometer
 NASA    - National Aeronautics and Space Administration
 NSA     - Northern Study Area
 ORNL    - Oak Ridge National Laboratory
 PANP    - Prince Albert National Park
 RSS-12  - Remote Sensing Science Team 12
 SSA     - Southern Study Area
 TM      - Thematic Mapper
 TMS     - Thematic Mapper Simulator
 TOMS    - Total Ozone Mapping Spectrometer
 URL     - Uniform Resource Locator
 UTC     - Universal Time Code

20. Document Information

20.1 Document Revision Dates

     Written:         07-Jan-1997
     Last Updated:    04-May-1998

20.2 Document Review Dates

     BORIS Review:    19-May-1997
     Science Review:  27-Jun-1997

20.3 Document ID

20.4 Citation

Please acknowledge the NASA/ARC investigation (RSS-12) and Michael Spanner, 
Principal Investigator, if these data are used or referenced. If appropriate, 
the references cited in Section 17 may be used.

20.5 Document Curator

20.6 Document URL

Keywords
---------------
Aerosols
Optical Thickness
Ozone


RSS12_Air_Sunphoto.doc
05/26/98