CALIPSO

Science Validation Plan

PC-SCI-501

 

 

 

 

 

 

 

 

 

 

 

 

Dave Winker and Chip Trepte

NASA Langley Research Center, Hampton, Virginia

 

Jacques Pelon and Anne Garnier

Institut Pierre Simon LaPlace, Paris, France

 

Tom Kovacs

Hampton University, Hampton, Virginia

 

 

 

 

 

 

 

Version 4.0

December 2004

 

 


TABLE OF CONTENTS

 

1 INTRODUCTION............................................................................................................................................................................................. 3

1.1 Purpose.................................................................................................................................................................................................. 3

1.2 Scope....................................................................................................................................................................................................... 3

1.3 Applicable Documents................................................................................................................................................................ 3

1.4 Revision History............................................................................................................................................................................... 4

1.5 Acronyms and Abbreviations Glossary......................................................................................................................... 5

2 BACKGROUND.............................................................................................................................................................................................. 7

2.1 Mission Overview............................................................................................................................................................................ 7

2.2 Science Objectives........................................................................................................................................................................... 7

2.3 Instruments and Measurements......................................................................................................................................... 8

2.4 Aqua Constellation and Orbit Information.............................................................................................................. 9

2.5 Science Data Products............................................................................................................................................................... 9

2.6 Success Criteria............................................................................................................................................................................ 10

3 VALIDATION APPROACH...................................................................................................................................................................... 11

3.1.1 Calibration and Characterization............................................................................................................................. 11

3.3.1 Field Campaigns......................................................................................................................................................................... 11

3.1.2 Algorithm Evaluation................................................................................................................................................................ 12

3.1.3 Correlative Measurement Planning........................................................................................................................................ 12

3.1.4 Correlative Instrument Development and Characterization.............................................................................................. 12

3.2 On-orbit Validation................................................................................................................................................................... 13

3.2.1 Level 1 Data Products................................................................................................................................................................ 14

3.2.2 Level 2 Aerosol Products........................................................................................................................................................... 16

3.2.3 Level 2 Cloud Products............................................................................................................................................................. 19

3.3 Correlative Data Sources..................................................................................................................................................... 22

3.3.1 Field Campaigns......................................................................................................................................................................... 23

3.3.2 Ground-based Measurements................................................................................................................................................... 26

3.3.3 Satellite Comparisons................................................................................................................................................................ 29

3.3.4 Data Assimilation and Models................................................................................................................................................. 30

3.4 Data Access Policy...................................................................................................................................................................... 30

3.5 Data Ingest and Display Tools........................................................................................................................................... 31

4. IMPLEMENTATION SCHEDULE............................................................................................................................................................ 32

4.1 Data Release Requirements.................................................................................................................................................. 32

4.2 Satellite Assessment Phase (L+0 to L+40 days)........................................................................................................... 32

4.3 Initial Instrument Validation (L+40 days to L+135 days).................................................................................... 33

4.4 Primary Validation Phase (L+135 to L+18 months).................................................................................................... 34

4.5 Continued Data Assessment Phase (post L+18 months)........................................................................................ 35

4.6 CALIPSO Validation Milestones (referenced to Launch Readiness Date)................................................. 35

5. MANAGEMENT........................................................................................................................................................................................... 35

6. Contact Information..................................................................................................................................................................... 36

 


1 INTRODUCTION

1.1 Purpose

 

The Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observations (CALIPSO) Validation Plan provides an overview of the requirements and approach for validating Level 1 and Level 2 science data products from the CALIPSO satellite mission.

 

1.2 Scope

 

This validation plan addresses pre-launch and post-launch activities for validating the Level 1 and Level 2 Science Data Products of the CALIPSO satellite mission. The document provides an overview of the mission objectives and payload instrumentation in section 2. General information and procedures for calibration and validation of the data products are described in section 3. These are followed with specific implementation plans for the three validation phases of the mission in section 4 and identification of primary oversight responsibilities in section 5. As they are part of the CALIPSO Science Data Products, but are defined as level 4 products, only a brief discussion is provided in this document for the validation of surface and atmospheric fluxes products retrieved using combined CERES and CALIPSO observations. These plans are further detailed in the CERES SARB Validation Plan.  Plans are not included in this document for validating other products derived from synergistic algorithm retrievals with measurements from other satellite platforms in the A-Train constellation. Details on pre-launch and in-flight instrument calibration activities are described in the CALIPSO Algorithm Theoretical Basis Documents C-SCI-201 and C-SCI-203. Routine quality assurance and algorithm improvement activities are not covered in this plan.

 

1.3 Applicable Documents

 

PC-SYS-101                     Science and Mission Requirements Document

PC-SCI-201                      Algorithm Theoretical Basis Document Lidar Level 1

PC-SCI-202                      Algorithm Theoretical Basis Document Lidar Level 2

PC-SCI-203                      Algorithm Theoretical Basis Document IIR Level 1

PC-SCI-204                      Algorithm Theoretical Basis Document IIR Level 2

PC-SCI-205                      Algorithm Theoretical Basis Document WFC Level 1

PC-SCI-503                      CALIPSO Data Products Catalogue

PC-SCI-504                      Quid Pro Quo Validation Plan


1.4 Revision History

 

This plan will be updated periodically, or as warranted by instrument or algorithm developments or by changes in comparison strategies.

 

Release Version                                    Date

 

Version 0.7                        December 2002                       Preliminary draft

Version 0.8                        February 2003                         Preliminary draft

Version 1.0                        April 2003                                Baseline plan

Version 2.0                        January 2004                            Updated information

Version 3.0                        July 2004                                 Updated information

Version 4.0                        December 2004                       Updated information


1.5 Acronyms and Abbreviations Glossary

 

AATS              Ames Airborne Tracking Sunphotomer

AD-NET          Asian Dust Network

AERONET     The Aerosol Robotic Network

AIRS               Atmospheric Infrared Sounder

AMMA            African Monsoon Multidisciplinary Analyses

ARM               Atmospheric Radiation Measurement

ATBD              Algorithm Theoretical Basis Document

ASDC              Atmospheric Sciences Data Center

AVE                Aura Validation Experiment

BSRN              Baseline Surface Radiation Network

CALIOP          Cloud and Aerosol Lidar with Orthogonal Polarization

CALIPSO        Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observations

CERES            Clouds and the Earth’s Radiative Energy System

CMDL             Climate Monitoring and Diagnostic Laboratory

CNES              Centre National d’Etudes Spatiales

CNRS              Centre National de la Recherche Scientifique

DEM                Digital Elevation Maps

DIRAC            IIR instrument simulator           

EARLINET     European Aerosol Research Lidar Network

GLAS              Geoscience Laser Altimeter System

GMAO            Global Modeling and Assimilation Office

GPS                 Global Positioning System

HSRL              High Spectral Resolution Lidar

ICESAT           Ice, Cloud and Land Elevation Satellite

IIR                   Imaging Infrared Radiometer

INTEX             Intercontinental Chemical Transport Experiment

IPSL                Institut Pierre Simon Laplace

IRR                  Infrared Imaging Radiometer

IWC                Ice Water Content

LAABS            Langley A-Band Spectrometer

LEANDRE      Multi-Wavelength airborne Backscatter Lidar (IPSL)

LITE                Lidar In-Space Technology Experiment

LNG                LEANDRE New Generation

LOA                Laboratoire d’Optique Atmosphérique

MAS                MODIS Airborne Simulator

MISR               Multi-Angle Imaging Spectro-Radiometer

MODIS           Moderate Resolution Imaging Spectroradiometer

MSG                Meteosat Second Generation

NASTI             NPOESS Airborne Sounding Testbed Interferometer

NASA             National Aviation and Space Administration

NDSC             Network for the Detection of Stratospheric Change

OMI                Ozone Measuring Instrument

PARASOL      Polarization and Anisotropy of Reflectances for Atmospheric Sciences coupled with Observations from a Lidar

PDF                 Probability Distribution Functions

POAM             Polar Ozone and Aerosol Measurement

POLDER         POLarization  and Directionality of Earth Reflectances

QPQ                Quid Pro Quo

REALM           Regional East Atmospheric Lidar Mesonet (REALM).

SAGE              Stratospheric Aerosol and Gas Experiment

SARB              Surface And Atmospheric Radiation Budget

SEVIRI            Spinning Enhanced Visible and Infrared Imager

SMRD             Science and Mission Requirements Document

SNR                Signal-to-Noise Ratio

SURFRAD      Surface Radiation Budget Network

TBD                 To be determined

WCRP             World Climate Research Program

WFC               Wide Field Camera

WRS                World Reference System

 


2 BACKGROUND

2.1 Mission Overview

 

Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observations (CALIPSO) is a satellite mission designed to measure the vertical structure and optical properties of aerosol and clouds over the globe that are needed to better understand their role in the climate system.  This knowledge will lead to improvements in our ability to model and predict climate variability and long-term climate change. The mission is co-sponsored by the United States’ National Aeronautical and Space Administration (NASA) and France’s Centre National d’Etudes Spatiales (CNES).

 

The CALIPSO payload consists of three instruments: a two-wavelength polarization-sensitive lidar referred in the remainder of this document as the Cloud and Aerosol Lidar with Orthogonal Polarization (CALIOP); a three-wavelength Imaging Infrared Radiometer (IIR); and a single-channel visible imager or Wide Field Camera (WFC). This suite of instruments will be placed in a sun-synchronous orbit and will fly in formation with the Aqua satellite constellation (e.g., Aqua, CloudSat, CALIPSO, PARASOL, and Aura satellite missions) to obtain near-coincident measurements with active and passive instruments on these other platforms. The CALIPSO mission is scheduled for launch (with CloudSat) during the summer of 2005 and has a planned operational lifetime of 3 years.

2.2 Science Objectives

 

Aerosols directly affect the Earth’s energy balance by scattering and absorbing shortwave solar radiation, and by absorbing and emitting longwave infrared radiation. They can also indirectly affect this balance by influencing the properties and process of clouds though their role as cloud condensation nuclei. Aerosols further play a significant role in the chemical evolution of trace gases and pose serious air quality and health concerns when concentrations are large. The physical and optical properties of aerosols are complex and vary considerably due to differences in composition, sources, and environmental conditions.

Model estimates of global aerosol radiative forcing are highly uncertain, largely because observations are insufficient to constrain or verify key assumptions in these models. Synergistic measurements from the A-train will enable the first observationally based estimate of direct aerosol forcing. The CALIPSO mission will provide profiles of aerosol backscatter and extinction coefficients over the globe.  Its multi-spectral and polarization measurements will further provide height-resolved information on aerosol type. These measurements will be combined with near simultaneous measurements from A-train instruments of aerosol optical parameters (i.e., MODIS, OMI, and PARASOL), atmospheric state (e.g., AIRS, MLS), and radiative fluxes (CERES) to provide estimates of direct aerosol forcing and key independent variables that control it.

Understanding the effects of clouds on Earth’s radiation balance, and particularly on longwave fluxes within the atmosphere and at the surface, depends on having accurate knowledge on the location of clouds vertically within the atmosphere and their multi-layer structure as well as having knowledge of their phase and ice/water content. Coincident profile information from CALIPSO’s lidar and from CloudSat’s radar offers a unique opportunity to map the vertical structure of clouds over the globe with accuracy never before realized. The combination of these data with observations from other A-train instruments (e.g., MODIS, CERES, and PARASOL) will provide more accurate measurements of surface longwave fluxes and atmospheric heating rate profiles that are needed to improve weather forecasting and climate prediction.

The CALIPSO mission will also provide new observations on cloud physical and optical properties that are needed to better understand cloud feedback processes. Presently, the largest uncertainties in predicting climate are associated with modeling a variety of cloud-radiation-climate feedback processes.  Because of the short time scales and nonlinear relationships typical of cloud processes, the only way to verify the representation of these processes in models is with nearly simultaneous observations of atmospheric state, cloud physical and optical properties, and of the radiation field.  Observations from CALIPSO and the other satellites of the A-train will provide an unprecedented suite of measurements to investigate these complex processes.

2.3 Instruments and Measurements

 

The CALIPSO instrument payload is designed to operate autonomously and continuously. The CALIOP laser transmitter subsystem consists of two redundant lasers, each with a beam expander, and a beam steering system. The Nd:YAG lasers are diode-pumped and operate at 1064 nm and 532 nm with a pulse repetition rate of 20.25 Hz.  Beam expanders are used to reduce the angular divergence of the laser beam to a diameter of 70 meters at the Earth’s surface.  The lidar receiver subsystem is designed to measure the backscattered intensity at 1064 nm and the two orthogonal polarization components at 532 nm  (parallel and perpendicular to the polarization plane of the transmitted beam).  This subsystem consists of the telescope, relay optics, detectors, preamps, and line drivers mounted on a stable optical bench. A fixed field stop located at the telescope focus defines the 130 µrad field of view.  A narrowband etalon is used in the 532 nm channel to reduce the solar background illumination.  A dielectric interference filter provides sufficient solar rejection for the 1064 nm channel.  Dual digitizers on each channel provide the effective 22-bit dynamic range needed to measure both cloud and molecular backscatter signals. An active boresight system is used to ensure co-alignment between the transmitter and the receiver.

 

The fundamental sampling resolution of CALIOP is 30 meters vertical and 333 meters horizontal, which is determined by the receiver electrical bandwidth and the laser pulse repetition rate.  Backscatter data will be acquired from the surface to 40 km.  Because of limitations to the downlink telemetry bandwidth, lidar profiles will be averaged on-board both vertically and horizontally to reduce the data volume.  This averaging will begin in the upper troposphere and extend upwards into the stratosphere. In this region, lidar profiles will be reduced to a vertical resolution of 60 m and a horizontal resolution of 1 km. In the stratosphere, the profiles will be further degraded to a vertical resolution of 180 m and a horizontal resolution of 5 km.

 

CALIOP profiles will be calibrated by normalizing the return signal to the predicted backscatter coefficients derived from meteorological observations in the aerosol-free region between 30 km and 35 km.  On-board calibration hardware will be used to calibrate the 532 nm perpendicular channel relative to the 532 nm parallel channel.  The 1064 nm channel will be calibrated relative to the 532 nm total backscatter signal using optically thick cirrus clouds as reference targets.

 

The IIR and WFC instruments are both nadir viewing and co-aligned with the lidar. The IIR provides calibrated radiances at 8.65 mm, 10.60 mm, and 12.05 mm over a 64 km swath, with a spatial resolution of 1 km.  Spectral bandwidths are respectively 0.9 mm, 0.6 mm and 1 mm. These spectral characteristics were chosen to optimize joint lidar/IIR retrievals of cirrus emissivity and particle size.  The IIR detector consists of a microbolometer array in a non-scanning, staring configuration, which allows for a simple and compact design. For on-orbit calibration, the IIR will use a dual approach that views either a temperature-monitored black body source or deep space. Independent comparisons will also be made with calibrated measurements from ground-based and airborne sensors.

 

The WFC consists of a single channel covering the 620 nm to 670 nm spectral region and provides images with a 61 km swath and a pixel resolution of 125 m.   The WFC provides meteorological context for the lidar measurements and allows highly accurate spatial registration, when required, between CALIPSO and instruments on other satellites of the Aqua constellation.  WFC data will be acquired only during daylight conditions and will be used for the retrieval cloud properties.

 

2.4 Aqua Constellation and Orbit Information

 

CALIPSO will be flown as part of the Aqua satellite constellation (or A-train), which consists of the Aqua, CloudSat, CALIPSO, PARASOL, and Aura satellite missions.  The constellation has a nominal orbital altitude of 705 km and inclination of 98o.  Aqua will lead the constellation with an equatorial crossing time of about 1:30 PM. CloudSat and CALIPSO will lag Aqua by 1 to 2 minutes and will be separated from each other by 10 to 15 seconds. PARASOL is planned to fly ~2 minutes behind CALIPSO. Aura will be last in the formation separated from Aqua by about 15 minutes. 

 

For the first 2 years of the mission, the nadir track of CALIPSO and CloudSat will be offset eastward from the Aqua nadir track by approximately 215 km at the equator. This shift permits comparisons with MODIS aerosol products in regions that would have been otherwise masked by sun glint during the northern hemispheric summer. During the third year of the mission, the current plan is to allow CALIPSO to precess westward across the swath of MODIS and CERES to view aerosol and cloud properties at a variety of viewing angles.

 

The satellites in the A-train will be maintained in orbit to match the World Reference System 2 (WRS-2) reference grid. This reference system was developed to facilitate regular sampling patterns by remote sensors in the Landsat program. Each satellite will complete 14.55 orbits per day with a separation of 24.7o longitude between each successive orbit at the equator. The orbit tracks at the equator will progress westward 10.8 o on succeeding days, which over a 16-day period, will produce a uniform WRS grid over the globe. The WRS grid pattern consists of 233 orbits with separation between orbits at the equator of 172 km. The Aqua satellite will be controlled to the WRS grid to within +/- 10 km. Additional information on the WRS can be obtained at: http://landsat.gsfc.nasa.gov/documentation/wrs.html

 

2.5 Science Data Products

 

The CALIPSO Level 2 Science Products are defined in the Algorithm Theoretical Basis Documents (ATBD) and are listed in detail in the Data Products Catalogue (PC SCI 503). These products will be produced and archived at the Langley Atmospheric Sciences Data Center (ASDC). Table 1 gives a summary of the CALIPSO Level 2 data products and the spatial scales at which the data products will be reported.  The expected accuracies given are for the maximum averaging distances for which the products will be retrieved. Cloud products will be reported at a horizontal resolution of 5 km; i.e., at the fundamental averaging resolution of the processing scheme. Cloud boundaries, which can be detected at higher resolution, will be reported at that resolution.  To account for weaker backscatter signals from aerosols, the Level 2 aerosol profile products will be reported at a uniform horizontal resolution of 40 km at all altitudes.

 

 

Table 1. CALIPSO Level 2 Aerosol and Cloud Measurements

 

Data Product

Measurement Capabilities and Uncertainties

Data Product Resolution

Horizontal

Vertical

Aerosols

Height, thickness

For layers with b > 2.5 x 10-4 km-1 sr-1

5km

60 m

Optical depth, t

40% *

5 km

N/A

Backscatter, b a(z)

20 - 30%

40 km

40 km

Z < 20 km 120 m

Z ³ 20 km: 360 m

Extinction, sa(z)

40 % *

40 km

40 km

z < 20 km  120 m

z ³ 20 km: 360 m

Clouds

Height

For layers with b > 1 x 10-3 km-1 sr-1

 

1/3, 1, 5 km

30, 60 m

Thickness

for layers with t < 5

1/3, 1, 5 km

 

30, 60 m

Optical depth, t

within a factor of 2 for t < 5

5 km

N/A

Backscatter, b c(z)

20 - 30%

5 km

60 m

Extinction, sc(z)

within a factor of 2 for t < 5

5 km

60 m

Ice/water phase

Layer by layer

5 km

60 m

Ice cloud emissivity, e

±0.03

1 km

N/A

Ice particle size

±50% for e > 0.2

1 km

N/A

Note: * assumes 30% uncertainty in the aerosol extinction-to-backscatter lidar ratio, Sa

 

 

2.6 Success Criteria

 

The CALIPSO science data products are considered to be validated if either the uncertainty estimates for the geophysical products have been shown to hold, based on comparisons with independent data products of high quality that have already been validated themselves, or the discrepancies between such comparisons have been understood and explained. A goal of the validation effort is to provide the user community with sufficient information to explain the quality of the data, in terms of precision and relative accuracy, and the spatial/temporal variations in these quality attributes.

 

 

 

 

3 VALIDATION APPROACH

 

For the CALIPSO mission, validation is defined as an assessment of the accuracy and precision of the derived science products by independent means. This includes an end-to-end understanding and characterization of the instrument, algorithms, and databases that will be used to generate data products and estimates of their uncertainties. It also includes activities that verify whether the data products are of sufficient quality to address its primary science objectives. Validation of Level 1 data products focuses on the calibration and verification of instrument performance (e.g., SNR, linearity) and the algorithms used for geolocation and lidar altitude registration.  Validation of Level 2 data products is concerned with the quantification of the random and bias errors in the data products, as well as verifying the underlying assumptions on which the retrieval algorithms are based.

 

Validation of Level 2 products requires comparisons with independent measurements.  Independent measurements of CALIPSO Level 2 parameters are required as well as of parameters on which the CALIPSO retrievals depend, such as aerosol or cloud lidar ratio.  “Independent” is understood to mean that the measurements used for validation are direct or at least do not rely on the same assumptions as the CALIPSO retrieval algorithms.

 

Because the CALIPSO instruments have very narrow measurement swaths, spatial coincidence between measurements from validation instruments and CALIPSO is not guaranteed and consideration must be given to spatial matching of the measurements relative to the spatial variability of the aerosols and clouds sampled.  Inter-comparisons with measurements from other satellites, particularly other satellites in the A-train, are attractive in that a large, global set of coincident data can be obtained.  However, care must be taken to understand the measurement uncertainties and limitations of the retrieval techniques used to derive the parameters being inter-compared with CALIPSO data products. It should be noted that for some Level 2 products, such as ice water content, comparison data sets are difficult to obtain. For these products, validation will be based mostly upon consistency checks.

 

This chapter provides an overview of the validation approach adopted for the CALIPSO mission with a general discussion on the strategy and concerns. Details on the validation schedule and specific measurement activities are provided in Section 4.

 

3.1 Pre-launch Activities

3.1.1 Calibration and Characterization

The accuracy and precision of retrieved science measurements depends critically on knowledge of the payload instruments response to incident radiation. It is the objective of pre-launch instrument characterization and calibration activities to quantify the response of CALIOP, the WFC, and the IIR over a range of operating conditions to very precise levels. These activities will include measurements of the linearity and transient recovery of the detector system.  Atmospheric tests were conducted for the lidar system before payload integration (completed December 2003) to verify the boresight mechanism and obtain some information on instrument performance. Another set of measurements are planned at the launch site (scheduled for April 2005). For the IIR, pre-launch activities included characterization of the absolute radiometric response of the IIR referenced to a standard laboratory source. Measurements also included an assessment of the spectral transfer function of each IIR channel and characterization of the linearity of the detectors.. Calibration procedures are detailed in a CNES Ground Calibration Specifications Document. The IIR calibration performance budget is described in a document that will be issued by CNES after checkout activities. No pre-launch atmospheric testing activities for the IIR or WFC are planned.

 

3.1.2 Algorithm Evaluation

Pre-launch validation activities will include the use of simulated CALIOP, IIR, and WFC observations to test algorithms and data handling software. Simulated data sets derived from observational data sets such as the Lidar In-Space Technology Experiment (LITE) and the ER-2 aircraft Cloud Profile Lidar (CPL) and MODIS Airborne Simulator (MAS) instruments that were deployed during SAFARI 2000 and CRYSTAL-FACE are used to represent the characteristics of the CALIPSO instrument suite and the expected observed atmospheric variability. Algorithm retrieval studies will be conducted using these data sets to test performance. Simulated data sets will be also generated using prescribed aerosol and cloud characteristics as inputs to CALIOP and IIR instrument forward models. In this manner, Level 1 and 2 retrieval algorithms will be tested for a variety of realistic atmospheric conditions and instrument settings.

 

The science data processing software undergoes multiple tests as part of the development process as well as formal acceptance tests after the implementation of all major software revisions. Information on the software development activities, verification studies, and quality assurance plans are found in the Quality Assessment plans in the Data Management Plan (PC-SCI-502).

 

3.1.3 Correlative Measurement Planning

Plans for acquiring correlative measurements have been developed during the pre-launch phase and include the identification and establishment of agreements with cooperative ground-base measurement facilities under the Quid Pro Quo (QPQ) Validation Plan, development of a QPQ validation website (http://calipsovalidation.hamptonu.edu), and the development of plans for dedicated aircraft flights and integration of measurement requirements in international field campaigns.  Additional studies include the preparation of statistical analysis and data assimilation techniques. 

 

3.1.4 Correlative Instrument Development and Characterization

To a large degree, the CALIPSO validation program will be built upon comparisons from well characterized and understood instruments with long measurement records. Validation of some of the CALIPSO products, however, requires additional correlative information that exceeds the capabilities or availability of these resources. To satisfy these needs, several instrument systems are either under development or modification that are aimed at supporting CALIPSO validation. For CALIPSO lidar products, two new airborne High Spectral Resolution Lidar (HSRL) systems are being developed: one by NASA LaRC and another by IPSL. These instruments will complement airborne elastic lidar systems operating at similar wavelengths, which by themselves can satisfy a number of correlative measurement requirements for CALIOP.  However, for the validation of backscatter and extinction profile measurements, additional information is needed. This is necessary because the retrieval of these products from backscatter lidar measurements requires a priori knowledge of a backscatter-to-extinction coefficient, also known as the lidar ratio.  The lidar ratio, which is noted for aerosols as Sa and clouds as Sc, depends on particle size, composition, and shape and can vary by a factor of ~5 or more. The distribution of Sa is poorly known and is a major source of uncertainty in the retrieval of extinction, perhaps as large as 30%. Knowledge of Sc is also important for clouds of intermediate optical thickness.

 

Several ground-based Raman and HSRL lidars have been operational for a number of years and provide unambiguous measurements of the altitude resolved backscatter coefficient, extinction, and the lidar ratio. To improve matching criteria between satellite and correlative sensors, similar airborne lidars are desired for CALIPSO validation. Unfortunately, construction of an airborne Raman lidar system operating at a wavelength of 532 nm is not practical because of the poor sensitivity of its cross section. Improved signal-to-noise can be achieved with higher transmission power, but only at levels that are not eye-safe for ground and airborne observers. The alternative HSRL systems operating at the same wavelength, on the other hand, are ~1000 times more sensitive and are eye-safe.  

 

For these reasons, compact HSRL systems are currently under development by NASA LaRC and IPSL. These systems will be deployed on aircraft to provide correlative measurements along the CALIPSO ground track. IPSL’s LEANDRE New Generation (LNG) lidar provides depolarization and high spectral resolution measurements at 355 nm. The instrument also operates as a conventional elastic lidar at 532 nm and 1064 nm. NASA’s HSRL provides depolarization and high spectral resolution measurements at 532 nm.  It also provides elastic backscatter and depolarization measurements at 1064 nm. Measurements from these instruments should greatly aid in the determination of uncertainties with CALIPSO’s aerosol and cloud retrievals. Developing an inventory of Sa by location, altitude, and season will also be valuable for other elastic lidar systems such as GLAS.

 

To support validation of the CALIPSO IIR, two airborne infrared sensors are planned to be operated by French scientists. IPSL’s DIRAC instrument is a CALIPSO IIR simulator with 4 spectral channels that uses rotating filters (3 channels matched to the CALIPSO IIR and a fourth channel matched to the 11 mm channel on MODIS) and uses the same micro-bolometer detector array design as the CALIPSO IIR. CLIMAT (developed by LOA and CIMEL) is a narrow FOV IR radiometer that also acquires measurements at the same 3 spectral channels as CALIPSO. These instruments can be further complemented by a 5-channel mid-IR radiometer with measurement of the polarized reflectance at 1.6 mm and 2.2 mm to retrieve the effective size of ice crystals.  All of these instruments have undergone preliminary testing and are expected to be flown in concert with IPSL’s HSRL (LEANDRE New Generation (LNG)) during validation flights. A visible camera will also be included to simulate the full CALIPSO instrument payload.

 

In addition to these airborne instruments, IPSL is developing a couple of mobile remote sensing facilities for clouds and aerosols.  One of these systems, Transportable Remote Sensing Station (TreSS), has been developed at LMD and will include a 2 wavelength, depolarization mini-lidar, an IR radiometer with spectral bands covering 9.5 – 11.5 mm, a pyranometer, and a 4-channel sunphotometer. The intent is to deploy the facilities under CALIPSO ground-tracks, thereby, improving comparison opportunities with well-matched observations.

 

3.2 On-orbit Validation

 

Comparisons with correlative measurements obtained from well-characterized instruments will serve as the primary basis for evaluating the relative accuracy of the derived data products.  Self-consistency analysis, limit checks, and sensitivity analysis will also be used to evaluate instrument performance and data uncertainties.

 

The difference between two measurements that are not exactly collated in space or time or have different resolutions will include some measure of geophysical variability, which is unrelated to measurement uncertainty. Where matching errors are small relative to the spatial correlation scales, validation can be done by direct inter-comparison of measurements.  In other cases, averaging and other statistical techniques can be used to reduce uncertainties due to matching errors to reveal the errors due to measurement and retrieval.  Comparisons with observations from long-term ground stations can also be performed, where regional statistics from CALIPSO are compared with local statistics compiled over a long time period.

 

The deployment of correlative instruments on aircraft platforms during field campaigns allows co-location with CALIPSO measurement locations. Field campaigns can also contribute to validation through the use of instrument simulators.  CALIPSO retrievals will be tested on data acquired both before and after launch by airborne simulators.  With proper experiment design, these retrievals can be validated using other data acquired during the field campaign.  This approach minimizes many of the sampling issues involved in inter-comparing validation data with CALIPSO observations themselves.

 

Specific validation approaches are identified for the various products listed below. Included in the discussion are suggested guidelines on matching criteria and techniques for correlative measurements.

 

3.2.1 Level 1 Data Products

The primary validation tasks for Level 1 data products include verification of geolocation, assessment of pointing biases, and evaluation of on-orbit calibration.  This activity will include an assessment of the instrument signal-to-noise ratio (SNR), linearity, as well as radiometric calibration.

 

Lidar footprint geolocation and altitude registration:  Altitude registration can be verified through comparisons between the measured altitude of the ocean surface with estimates computed using satellite ephemeris and attitude data. The geolocation of the lidar footprint can be verified through comparisons with surface Digital Elevation Maps (DEM). The CALIPSO geolocation requirement is for the lidar footprint to be co-located within a 1 km resolution pixel observed by MODIS on Aqua.  The GTOPO30 DEM from the U.S. Geological Survey is a possible reference source with a spatial resolution of approximately 30 arcsec (~1 km at equator) and vertical resolution of 30 m. Digital maps from the Space Shuttle Radar Topography Experiment provide an alternative data source with superior spatial resolution (horizontal resolution 30 m and vertical resolution of 5-10 m); however, this coverage currently extends only over the continental United States. Location errors and pointing biases will be determined from differences between the lidar surface return height and the DEM data at the footprint locations.

 

Imager pixel geolocation: The geolocation of the IIR and WFC image pixels and their position relative to the lidar footprint will be evaluated both along and perpendicular to the spacecraft ground track through comparisons with identifiable, high contrast landmarks such as coastlines using high-resolution DEMs. This procedure has been widely used by other satellite experiments and is reviewed in the WFC ATBD.

 

Lidar profile calibration:  The 532 nm parallel channel will be calibrated in-flight by normalizing the backscatter coefficients above 30 km where molecular scattering dominates. Baseline subtraction, correction of baseline shape effects, and the on-orbit merging algorithm will be verified by looking at heavily averaged clear-air profiles (i.e., no aerosols). The 1064 nm channel will be calibrated through cross comparisons with the 532 nm backscatter observations from optically thick cirrus clouds.  The 532 nm perpendicular channel will be calibrated relative to the parallel channel using a pseudo-depolarizer, which can be inserted into the received beam on command.  Measurements of clouds having high and low depolarization with ground-based or airborne depolarization lidars can be used to check the calibration of the depolarization gain ratio and to assess uncertainties in the depolarization of the transmitted beam. Details of the lidar calibrations are contained in the lidar Level 1 ATBD.

 

IIR radiance calibration: The IIR will be calibrated in orbit employing sequential views of a temperature-monitored warm black body radiance source (~295 K) and deep space at ~4 K. These observations will allow determination of the detection gain and offset for each spectral channel and each pixel. Details of the IIR on-orbit calibration algorithm are described in the CNES IIR/Calipso Level 1 processing requirements. Calibrated radiances will be verified through consistency checks and direct and indirect comparisons. Both the radiometry and the spectral response of the three IIR channels have to be checked over a brightness temperature range of 220 to 310 K. As the solar reflectance should not impact radiances in the thermal IR region, both daytime and nighttime comparisons will be useful to identify biases. Initial calibration analysis will rely on vicarious comparisons of clear sky measurements over oceans.

 

In the level 2 IIR processing algorithm, the IIR radiances (brightness temperatures) utilize comparisons with radiative transfer model computations under clear sky and dense cloud conditions. It relies on the use of operational atmospheric profiles (temperature and humidity) and surface conditions (temperature and emissivity).  CALIOP observations are used to identify clear sky pixels along the satellite track. For data processing activities, temperature and humidity profiles will be obtained from operational GMAO meteorological products. For special comparison studies, coincident radiosonde profile measurements will be required. Measurements over the ocean will require concurrent sea surface temperature from buoys or from satellite measurements such as AIRS/AMSU/HSB, MODIS, CERES or SEVIRI.

 

Comparisons of measured and calculated brightness temperatures over land are also -envisaged for homogeneous areas where the surface emissivity and temperature can be measured locally or from satellite measurements such as ASTER. Calibration studies over Polar Regions covered with ice or snow are of special interest. Comparisons with measurements from ARM and GEWEX field instrument sites at high and low latitudes are also desired because of the broad range in surface temperature. These sites are well established with long measurement records and include a variety of in situ and remote sensing instruments that are particularly valuable for IIR calibration studies. Several sites have up- and down-looking infrared radiometers over the same wavelength range as the IIR (9.6 to 11.5 mm). 

 

Direct comparisons with measurements from other instruments over a variety of atmospheric conditions will be conducted.  Measurements will be made above cloud scenes to ensure similar viewing to the IIR.  Plans are to acquire correlative measurements on-board the Falcon 20 aircraft with the DIRAC/CALIPSO instrument simulator and the CIMEL IR radiometer CLIMAT . This aircraft has a nominal flight service ceiling of 39,000 feet and should be sufficient to fly above mid altitude clouds in all seasons and cirrus in winter. Comparisons are being considered with MAS on the ER-2. Indirect comparisons with high spectral resolution IR spectrometers will permit an assessment of the unfiltered IIR spectra. Comparisons can be obtained with AIRS observations in the 8.8-15.4 mm region or with airborne measurements from the NPOESS Airborne Sounding Testbed Interferometer (NASTI). Ground-based up-looking AERI radiometers at the ARM sites may also be used under clear sky conditions, preferably in association with a backscatter lidar. In addition, standard resolution radiometers may provide valuable comparison observations. Examples include the DIRAC IIR simulator (when not involved in a field campaign) or the CIMEL IR radiometer CLIMAT, currently operated at the IPSL instrumental site near Paris (France). and up-looking IR radiometers covering the CALIPSO IIR channels

 

Direct comparisons are planned on a regular basis with simultaneously observing IR spectro-radiometers having similar channels: MODIS, AIRS, and CERES on AQUA and the SEVIRI imaging radiometer on the Meteosat Second Generation (MSG) spacecraft are being considered..  MSG was launched in August 2002 into a geostationary orbit stationed over Europe and Africa. Since SEVIRI collects measurements in 15-minute intervals, an assessment of uncertainties due to temporal sampling by CALIPSO will be possible.

 

WFC radiance calibration:  Calibration of the WFC will be based primarily upon vicarious comparisons with nighttime views of the Earth and daytime views of tropical deep convective clouds as standard dark and bright targets, respectively. Additional comparisons will be made with near-simultaneous MODIS observations. Details of the WFC on-orbit radiance calibration are covered in the WFC Level 1 ATBD.

 

3.2.2 Level 2 Aerosol Products

 

Aerosols have complex physical and optical properties that can vary with changes in environmental conditions. Observations suggest that coherent space and time scales for aerosol concentration are on the order of 100 km or less and range from minutes to hours, respectively. These scales place limits on matching requirements between correlative measurement activities and CALIPSO observations.  Greatest coincidence will be obtained with measurements from aircraft platforms deployed along the CALIPSO satellite orbit track and within a few minutes of its overpass. Coincidence opportunities for direct comparisons between CALIPSO observations and ground-based instruments, on the other hand, are not as straight forward.  A preliminary guideline for obtaining matched aerosol coincidences is for the CALIPSO ground track to pass within 100 km of an instrument site and within an hour of the satellite overpass. This guideline attempts to balance differing horizontal resolution scales for the CALIPSO data products against the limited matching opportunities available from other instruments with narrow field-of-views, while still ensuring that common aerosol structures are viewed by both measurement systems. For correlative measurements that do not fall within these match criteria, comparisons will be conducted based on ensemble averages and probability distributions.

 

Height and thickness:  Validation of the altitude registration is addressed in Level 1 activities. The primary concern for the validation of aerosol layer height and thickness, however, is in determining the detection limits of the CALIPSO aerosol/cloud detection algorithm. For this requirement, comparisons of aerosol layer height and thickness with correlative backscatter lidar profile measurements are needed for a variety of aerosol loadings (as well as a variety of cloud types and cloudiness). Ground-based and airborne backscatter lidar systems can provide the necessary correlative data.

 

Backscatter profile, extinction profile and optical depth:  The accuracy of retrieved profiles of aerosol backscatter, extinction and the column optical depth is dependent upon measurement uncertainties as well as the underlying assumptions of the retrieval algorithm.  For backscatter lidars such as CALIOP, the retrieval of these parameters relies heavily upon an estimation of Sa.  For elevated layers, the retrieval scheme determines optical thickness from the difference between the molecular backscatter above and below the layer. A layer-averaged Sa can be estimated from the measurement itself and the optical thickness is then used to constrain the retrieval of backscatter and extinction. For aerosol layers that are not elevated, the retrieval algorithm estimates Sa on the basis of aerosol type using a variety of information including the ratio between 532 and 1064-nm backscatter and the depolarization at 532 nm.

 

For validation of aerosol backscatter and extinction profiles at 532 nm, lidar observations offer the best opportunity for evaluating the accuracy of these products in the troposphere. Correlative measurements from established backscatter lidar sites such as those participating the European EARLINET program and the MPL network will be particularly valuable for placing CALIPSO measurements within the context of long and broad measurement records. Airborne backscatter lidar measurements (e.g., CPL) are also valuable for evaluating aerosol backscatter and extinction. As noted before, however, the retrieval of these products is highly dependent upon estimates of Sa, which can have uncertainties of perhaps 30%. One approach for obtaining a more self-consistent extinction measurement is to co-locate a multi-wavelength sun photometer and backscatter lidar so that estimates of Sa are constrained by column optical depth observations. This approach would be acceptable for layers that are homogenous, but would be less appropriate over an altitude range where Sa varies significantly. For these conditions, HSRL and Raman lidars are believed to be more advantageous because they provide unambiguous profile measurements of backscatter, extinction, and Sa over the entire column with vertical resolution of a few hundred meters. Differential height measurements of optical depth using airborne radiometers also provide a means for obtaining profiles of aerosol extinction.  These measurements have been made with considerable success in previous field experiments. However, they can extend only a limited horizontal range because of the time required for the aircraft to conduct spiral ascent or descent maneuvers.

 

For the validation of column aerosol optical depth, comparisons will be conducted with correlative measurements from surface and airborne multi-wavelength sun photometers and radiometers (e.g., AERONET and AATS-14). Comparisons with satellite retrievals of optical depth may also provide added insight. For example, in periods with aged, well-mixed volcanic aerosol conditions in the stratosphere, Sa is reasonably well known. Comparisons can be accomplished with satellite measurements from SAGE III, POAM III or MAESTRO, which provide extinction and optical depth products at similar wavelengths to CALIOP.  Additional direct and indirect comparisons between CALIPSO data sets and other ground-based instrument facilities and satellite measurements such as MODIS, MISR, OMI and GLAS will provide an understanding of relative biases and variations between data sets.

 

In addition to obtaining a limited set of coincident correlative measurements for CALIPSO to test aerosol retrievals, comprehensive measurements of Sa are needed to refine the algorithm that is used to select estimates of Sa. Measurements are needed that address the generalized aerosol types listed in Table 2. This objective would not necessarily require coincident measurements with CALIPSO and could be obtained from existing ground-based instrument facilities (as indicated in Table 2) or during airborne field missions.

 

 

Table 2.  Regions with Characteristic Aerosol Types of Particular Interest

with a few Representative Measurement Sites

Aerosol Type

Height/Thickness

ta

sa

Sa

Urban/polluted

Eastern U.S.

South America

Central Europe

 

 

 

 

China

 

India/Indian Ocean

 

Washington DC

Buenos-Aires

22 EARLINET sites,

 

 

Anhui Institute, CJFEPC

Pune

 

8 Aeronet sites

12 MFRSR sites

13 Aeronet sites

4 BSRN sites

Hamburg, Jungfraujoch, Kuehlungsborn, Leipzig, Palaiseau

 

6 Aeronet sites

 

Yulin, MALE, Kanpur

 

 

 

Kuehlungsborn, Leipzig

 

 

 

 

 

 

 

 

 

Kuehlungsborn, Leipzig

 

 

 

 

 

 

Biomass burning

South America

 

 

Southern Africa

 

Indonesia

 

Brasil

 

 

Reunion Island

 

Darwin

 

Alta Floresta, Cuiaba, Abracos Hill, Santa Cruz

Etosha Pan, Mongu, Skukusa

Darwin

 

 

 

 

Reunion Island*

Darwin*

 

 

 

 

Reunion Island*

Darwin

Desert dust

Saharan, southern Europe,and west

Asian and east

 

Tunisia, Italy

6 AD-NET sites, Suwon

 

Dakar

5 Aeronet sites

 

 

Nagoya*

 

 

Nagoya*

Polluted marine (sea salt, sulfate, soot)

Aberystwyth, Lisbon, Napoli, Okinawa

Okinawa, COVE, Kosan

Aberystwyth*, Napoli*

 

Dusty marine (sea salt, sulfate, dust)

Kyung Hee, Nagasaki

Capo Verde, Bermuda

Kyung Hee*

Kyung Hee*

Clean Continental

America, Europe

 

SGP, Haute Provence,

Minsk

 

Bratts Lake (Regina), Rimrock, Alice Springs, Pellston, Minsk

SGP (23 sites)

SGP*

SGP*

Clean Marine (sea salt)

Manus, Nauru, Mauna Loa, Dumont d’Urville, Ny Alesund

Manus, Nauru, Hilo, Mauna Loa, Tahiti, Kwajalein, Ny Alesund

Manus*,

Nauru*

Manus*, Nauru*, Mauna Loa*

Arctic haze

Barrow, Ny Alesund

Barrow, Atqasuk, Ny Alesund

Barrow

Barrow

 

An estimate of the multiple scattering parameter, h, is also needed for retrievals of aerosol (and cloud) extinction and optical depth. This parameter accounts for the apparent reduction in optical depth produced by multiple scattering and can be range-dependent.  One approach is to measure the aerosol phase function using a polar nephelometer and compute h using a multiple scattering code.  Although it is uncertain if polar nephelometers have sufficient sensitivity to provide the needed measurements.  The most promising technique for estimating h within aerosol layers is to compare lidar profiles from CALIPSO with a down-looking narrow-FOV aircraft lidar. The ratio of the normalized, range-corrected returns from these lidars can be taken as equivalent to the ratio of total scatter to single scatter and used to compute h directly.  An airborne multiple field-of-view lidar (e.g., CPL), which mimics the viewing geometry of CALIOP and also has a narrow field-of-view, would allow direct measurement of h appropriate for CALIPSO.

 

Table 3 summarizes the above discussion by listing the principal Level 2 aerosol data products and instruments that might be used to acquire inter-comparison data for validation, including tests of some of the underlying retrieval assumptions. A variety of other internal data products, not listed here, will be produced and used during data processing activities. Validation of these other products will rely on using CALIPSO products that have established levels of uncertainty or by inference. For example, backscatter color ratio profiles (ratio of backscatter profiles at 2 wavelengths) provide information on aerosol size distribution. A validation approach would be to compare these values with measurements on particle size from in situ particle samplers or derived from multi-wavelength observations from a sun photometer.

 

 

Table 3.  Correlative Measurement Requirements for Aerosol Products

Principal Parameters to be Validated

Candidate Comparison Instruments

layer height, thickness

 

G/B: backscatter lidar

A/C: backscatter, HSRL lidar

backscatter, b a(z)

extinction, sa(z)

lidar ratio, Sa (z)

A/C: HSRL, Raman lidar, 180-nephalometer

G/B: HSRL, Raman lidar, elevation-scanned backscatter lidar

optical depth, t

 

 

G/B: up-looking sun   photometer, radiometer,

airborne:  HSRL or Raman lidar

satellite:   e.g., MODIS, MISR, PARASOL, SAGE III, OMI

Sa  (layer averaged)

G/B: backscatter lidar & sun photometer

A/C: backscatter lidar & radiometer

satellite:  CALIPSO & PARASOL

multiple scattering parameter, h(z)

CALIPSO and airborne nadir viewing lidar

G/B = ground-based, A/C = aircraft

 

3.2.3 Level 2 Cloud Products

 

In contrast to tropospheric aerosols, clouds have relatively short lifetimes (often on the order of minutes to hours) and even shorter correlation spatial scales (a few kilometers to tens of kilometers). These constraints greatly complicate the validation of retrieved cloud properties by direct comparison with instruments at ground-sites. Because of the difficulty in obtaining large datasets of coincident aircraft measurements of different cloud types, it is also unlikely that a data set will become available from airborne measurement to comprehensively test Level 2 products. For these reasons, a more profitable validation approach is to acquire airborne measurements of a few critical parameters that may be directly compared with CALIPSO observations and rely on comparisons of measurement ensembles from different techniques, locations, and periods for other parameters. A similar approach is the basis of the CERES validation effort and is also being considered for CloudSat validation.

 

Comparisons with CALIPSO cloud retrievals under a variety of conditions are needed: water clouds, ice clouds, mixed phase clouds; optically thin and thick clouds; clouds with large and small particles; cirrus formed by various generating mechanisms at different latitudes (frontal, synoptic, anvil, etc).  Whether clouds are broken or overcast and single- or multi-layer is not so important from a retrieval point of view, but imposes different constraints on matching errors and suitability of comparison data.  It is also necessary to test cloud retrievals in a variety of climate regimes with varying cloud properties.  Since the deployment of field campaigns to all the regions of interest is not practical, efforts will be focused on a few major climate regimes.  For example, convective clouds and cirrus dominate a significant portion of the tropics, low altitude stratus or scattered cumulus exist over large portions of the marine subtropics, highly variable storm systems occur often in the mid latitudes, and a wide variety of ice and water clouds occur in the polar regions. 

 

Cloud height and thickness: Altitude registration issues are addressed by Level 1 activities.  The detection of clouds by lidar observations is largely a sensitivity issue, which is less critical for clouds than for aerosols because of the higher signal levels.  Direct comparisons with an airborne lidar and a high-resolution radiometer (e.g., DIRAC/LEANDRE and MAS/CPL) offers one of the best approaches for identifying cloud and aerosol features needed for verifying the CALIPSO cloud/aerosol detection algorithm. Preference is given to downward looking lidars because of cloud attenuation and to match the CALIPSO viewing volume. Insight on CALIOP detection thresholds for cloud bases may also be obtained through satellite data comparisons with MODIS cloud products. Coincident radar profile measurements from CloudSat will also be valuable for inter-comparing the height boundaries of clouds over the globe.

 

Cloud extinction profile and optical depth: Validation of cloud optical depth will primarily focus on comparisons using two different approaches. The first approach relies on measurements of solar radiance through clouds by upward-looking ground-based or airborne radiometers, while the second approach employs measurements of cloud transmission from ground-based and airborne lidars. Measurements from in situ particle samplers can provide estimates of both optical depth and extinction profiles.  However, in situ observations have sparse coverage because they require the aircraft to fly profile patterns and have added uncertainties associated with small sampling volume and calculations of extinction. Coincident A-train measurements will also provide powerful comparison opportunities. MODIS optical depth measurements will be extremely useful for single-layer cloud situations (as identified by CALIOP) and optimum sun angles. Additional cloud information will be available from CloudSat and PARASOL.

 

Profile measurements of Sc and h are also needed. For cirrus, estimates of Sc can be derived from direct cloud transmission measurements obtained from airborne lidar observations. Because of the small field of view of airborne lidar, this technique would have the added advantage of having reduced multiple scattering effects, allowing for an assessment of the magnitude of h for clouds. A layer-average Sc can be estimated from measurements from a sun photometer optical depth and backscatter lidar; however, sun photometer optical depth must be corrected for small-angle cirrus forward scatter.  As with aerosols, h could be assessed from direct comparison with aircraft lidar returns. Estimates of h are also available by indirectly measuring the cirrus phase function with in situ instruments including a polar nephelometer such as the one at LAMP in France and computing h through simulations.  An airborne multiple field-of-view lidar, which mimics the viewing geometry of CALIOP and also has a narrow field-of-view, which excludes multiple scattering, would allow direct measurements of h appropriate for CALIPSO (e.g. CPL, LNG).

 

Cloud ice/water phase and ice water content: It is expected that ground-based depolarization lidar observations will be useful for validation of CALIPSO depolarization profiles in the absence of low altitude clouds. Airborne depolarization lidar are preferred to reduce matching errors and increase observational capability.  For aircraft observations, down-looking lidar measurements are needed to validate CALIPSO cloud phase measurements for low altitude and optically thick clouds where the compensation for multiple scattering effects in the retrieval needs to be checked.  Direct in situ measurements of ice and water contents (e.g., Nevzorov sonde) can be useful in aiding the interpretation of depolarization lidar measurements.  Comparisons with MODIS and PARASOL ice/water phase products should prove to be useful in cases of single-layer or opaque cloud.

 

Cirrus emissivity and particle size: Effective emissivity, ec, of a semi-transparent upper cloud is calculated from the relationship, ec = (Li - Lo)/( (Lb - Lo), where Li is the upward radiance measured by the IIR, Lo is the outgoing sky radiance in the absence of the studied cloud layer, and Lb is the radiance from an opaque cloud at the radiatively equivalent temperature of the semi-transparent cloud.  For CALIPSO, ec and particle size data products for cirrus and other high altitude clouds will be derived from combined IIR radiances and lidar observations such as cloud height and depolarization characteristics for cloud systems having 1-3 layers. Extension across the swath will be derived from statistics on the homogeneity of the cloud field under the track combining IIR, lidar and WFC data for daytime periods. The algorithm uses ancillary data such as temperature and humidity profiles and surface emissivity and temperature. Validation of CALIPSO emissivity products will include comparisons from down-looking airborne instruments such as the combined DIRAC IIR simulator, LNG and visible camera instrument suite and dropsondes (when possible). It is also planned to make comparisons using an up-looking ground-based and radiosonde instrumentation on dedicated sites with characterized surface emissivity. Satellite comparisons of derived cloud products from MODIS or SEVIRI may also prove to be beneficial for single-layer cirrus scenes. It is planned also to check the emissivity retrieved over clouds identified as opaque by the lidar.

 

Comparison of cirrus particle size will be based largely on statistical comparisons with ground-based instruments such as multiple field of view lidars and either backscatter or Raman lidars combined with cloud profiling radars. As the robustness of the particle size retrieval depends upon both their size and shapes in relation with the wavelength range (between 8 and 12 mm), multi-instrumented sites with measurement in the visible, in the thermal IR and at larger microwave wavelengths can provide particle size measurements in complementary ranges. Airborne down-looking observations above the clouds using a multi-instruments payload such as the CALIPSO payload simulator, a cloud radar (operating at the same wavelength than Cloudsat), a mid-IR polarized radiometer and an airborne version of the radiometer/polarimeter POLDER would be therefore of great interest. Particle size and shape can be more directly measured with some accuracy using airborne in situ instruments, such as a Cloud Particle Imager, but there are several types of sampling difficulties, including the measurement sensitivity as a function of size and the very different sampling volumes between the in situ and satellite instruments. CALIPSO cirrus particle size can also be checked for consistency with satellite measurements in the A-train (for example comparing to retrievals from MODIS visible and near IR channels) or from SEVIRI. For the most part, particle size information will be retrieved only when the cloud emissivity ranges from ~0.1 to 0.9 (optically thin clouds) and the cloud layers are unambiguously identified.

 

Table 4 summarizes the above discussion by listing the principal Level 2 cloud data products and instruments that might be used to acquire inter-comparison data for validation, including tests of some of the underlying retrieval assumptions. The table also includes estimates on spatial matching requirements. As with aerosols, a variety of other data products not listed here will be produced.  Validation of these other products will generally be accomplished either by inter-comparing CALIPSO parameters with quantities derived from the basic validation measurements or by inference, when the quantities are derived from validated CALIPSO products.  In addition, there are a few derived products (cloud type, ice water content), which will need to be addressed specifically.

 

Table 4.  Validation Measurement Requirements for Clouds

Principal Parameters to be Validated

Horizontal Resolution Requirements

Candidate Comparison Instrument

cloud layer heights

20-50 km

backscatter lidar

optical depth, t

1-5 km

G/B*: radiometers/sun photometers

A/C*:  backscatter lidar, HSRL

Satellite: MODIS, PARASOL (single-layer clouds)

Sc,eff (layer-average)

~ 50 km

Backscatter lidar

spectral emissivity, e(li) (layer- average)

 

1-5 km

A/C: radiometers and backscatter lidar (DIRAC/LEANDRE; MAS/CPL)

Satellite: MODIS, AIRS, MSG/SEVIRI (single layer cirrus)

effective particle size, Deff

 

1-5 km

G/B and A/C: radiometers,  backscatter lidar with cloud-profiling radar,

A/C: in situ measurements,

Satellite : MODIS/AQUA, SEVIRI/MSG (few cases)

extinction profile, sc(z)

1-5 km

Raman lidar, HSRL, in situ samplers

lidar ratio profile, Sc (z)

1-5 km

Raman lidar, HSRL, in situ samplers

d(z)

1-5 km

Depolarization lidar

 ice/water phase

1-5 km

Depolarization lidar, G/B radiometer, MODIS, ASTER, PARASOL, in situ samplers

emissivity assumptions

1-5 km

P,T,U sounding, ASTER

multiple scattering parameter, h(z)

 

CALIPSO and airborne backscatter lidar

airborne multiple-field of view lidar (CPL, LNG)

* G/B = ground-based, A/C = aircraft

 

It is important to emphasize that, in addition to a variety of measurements intended to perform independent measurement of Level 2 parameters, it is also important to acquire airborne simulator data, which can be used as inputs to the retrieval codes.

 

3.3 Correlative Data Sources

 

This section provides an overview of the sources of correlative measurements utilizing instrument techniques identified above that may be available for CALIPSO validation. The primary source of data needed to test retrieval algorithms will be from of airborne measurement activities such as during the TC4 Costa Rica or TWP-ICE field experiments.  Over the lifetime of the CALIPSO mission, valuable correlative measurements will also be obtained from established ground-based instrument facilities around the globe that will be used to assess the relative accuracy of the retrieved data products. Comparisons with these observations will also permit an understanding of the context of CALIPSO’s measurements within the long-term aerosol and cloud observational records collected at many ground-based sites. Through these activities, satellite and ground-based remote sensing and in situ measurements can be integrated (employing suitable resources) to provide a more comprehensive data set needed to unravel the subtle relationships that control aerosol forcing.

 

Data from different measurement programs will be made available to the CALIPSO science team either through established validation or campaign archival sites (e.g., CRYSTAL-FACE, Aura Validation) or through the CALIPSO QPQ data depository.

 

3.3.1 Field Campaigns

Field campaigns are intensive observational activities that focus on specific objectives for brief periods and limited areas. Typically, the missions are designed to acquire a comprehensive set of observations that can explore atmospheric processes and support satellite validation activities in greater detail than available with conventional measurement programs. Over the next 5 years, NASA, CNES, and other international organizations are planning a variety of field missions that complement CALIPSO science interests and validation needs. It is through these measurement activities that many comparison activities will be realized. Members of the CALIPSO project and science team are engaged with program leaders of these different missions to help coordinate synergistic and correlative measurement opportunities.  Below is a listing of possible field missions, with information on their primary focus of interest. Information is also provided for each mission on types of measurements that would benefit either CALIPSO validation or related science studies.

 

Dedicated CALIPSO Aircraft Measurements: In the early phase of the mission, aircraft flights are required to obtain essential comparison data to help quickly assess the performance of the instruments and provide initial information on the accuracy of the retrieval algorithms.  Plans are to initially deploy both NASA’s and IPSL’s HSRL lidar systems on high altitude aircraft and fly along the satellite ground-track to examine Level 1 and a few Level 2 products. These will be complemented by elastic lidar cloud measurements from CPL over the tropics and mid latitudes. Coincident measurements from surface based and the NASA/AATS-14 and LOA/PLASMA airborne multi-channel sun photometers are also planned to obtain a complementary assessment on column optical depth or layer extinction. (see section 4.3 for more details).

 

Several other instruments will also be flown several months after launch to further analyze aerosol and cloud properties. IPSL’s DIRAC instrument and the CLIMAT IR radiometer have the same spectral channels as the IIR and will provide an opportunity for direct comparisons of spectral radiances as well as derived products.  The mid-IR polarized radiometer, the radiometer/polarimeter POLDER and various in situ measurements will provide a characterization of the cirrus ice crystals. RALI combines a Doppler radar with LNG to provide an instrument payload similar to that  employed by CALIPSO and CloudSat. RALI is also planned to be flown in France during this same period.. These validation flights will be aimed at acquiring various types of aerosol and cloud observations to test Level 1 and a subset of Level 2 retrievals.

 

 

Intercontinental Chemical Transport Experiment (INTEX) North America: The INTEX-NA field mission is designed to examine the composition and chemical evolution of tropospheric aerosols and trace gases that are exported to and from North America. The mission will take place in two parts. The first segment (Phase A) occurred during mid summer 2004 (before the launch of CALIPSO) and focused on the outflow of air originating over eastern North America. The second segment (Phase B) is planned for spring 2006 and will examine the composition of enhanced aerosols and trace gases entering North America that were exported from Asia and the central Pacific. These observations will lead to a better understanding of sources and sinks of climatically important trace gases and new insight into implications for surface air quality. The mission seeks to use the NASA DC-8 aircraft and coordinate flights with satellite overpasses. Coincident profile measurements of aerosol optical and physical properties, atmospheric state, radiation, and trace gases with satellite observations are needed to obtain a comprehensive assessment of the accuracy of the CALIPSO data products for aerosol forcing. This objective is consistent with the stated goals of the INTEX missions. (http://cloud1.arc.nasa.gov/intex-na/overview)

 

AURA Validation Experiment (AVE): AVE seeks to better understand the structure of the troposphere and the coupling between the troposphere and stratosphere. The mission is considering a combination of in situ and remote sensing instruments on a high altitude aircraft to:

 

-         Characterize the influx of material from the stratosphere into the troposphere,

-         Investigate relationship between ozone precursors and ozone production in the tropics and polluted regions,

-         Assess pollutant inflow and outflow over North America, and

-         Improve our understanding of convective detrainment of pollutants.

 

Aircraft flights will be coordinated to support Aura validation activities; and hence will complement other A-train elements such as CALIPSO validation and science studies.  AVE began in 2004 and is planned to conduct measurements through 2006.  Mission concepts seek to define a common instrument platform that participates in most observational sequences. For specific CALIPSO related science studies, measurements are requested that support further characterization of aerosol optical and physical properties (e.g., s and Sa), as well as composition, with concurrent observations of atmospheric state and radiative flux obtained under varying environmental conditions.

 

Tropical Composition, Cloud and Climate Coupling (TC4) or Tropical Clouds Systems and Processes (TCSP): TC4 seeks to quantify the transport, radiative, and chemical processes, and the coupling between these processes in the lower tropical stratosphere and the upper tropical troposphere (referred as the Tropical Tropopause Layer - TTL). A mission concept is being developed that will interweave Aura validation activities with specific process studies using a variety of high altitude aircraft/balloon platforms and ground-based instruments.  Different science goals include a better understanding of processes that control water vapor in the TTL and the formation and distribution of thin cirrus and their influence on radiative heating/cooling. The mission is also interested in obtaining an understanding the fates of short-lived compounds from the tropical boundary layer into the TTL as well as acquiring an understanding the mechanisms that control ozone in the tropical troposphere. The TC4 is being considered for mid summer 2005 with a base of operations in Costa Rica. The mission will partner with NASA’s CAMEX-5 study and NSF’s TEXMEX on the formation and evolution of tropical storms.

 

The Tropical Warm Pool-International Cloud Experiment (TWP-ICE): TWP-ICE will attempt to describe the evolution of tropical convection including the large-scale heat, moisture, and momentum budgets along with detailed observations of cloud properties and the impacts of the clouds on the environment.  An explicit objective of the experiment is to provide validation data for the A-train.  The experiment is a collaboration between the DOE ARM project, the Australian Bureau of Meteorology, NASA, the European Commission, and a number of universities.  The mission will be conducted from Darwin, Australia in January and February 2006 and will focus on convection during the Australian monsoon, which is believed to be representative of typical maritime convection in the tropics.  TWP-ICE will benefit from the likely participation of two other experiments: SCOUT-03 and ACTIVE, each planning to provide two aircraft instrumented to measure aerosols, clouds, and trace gases.

 

TWP-ICE plans to perform extensive characterization of tropical cirrus using both in situ and remote sensing aircraft.  The experiment will use a number of aircraft of various capabilities to conduct flight missions at low levels (< 5000 ft), mid-levels (15-30,000 ft) and high altitudes (50-60,000 ft).  Continuous measurements will be provided by the Darwin ARM site and a ship located about 200 km west of Darwin in the Timor Sea.  A high quality uplooking lidar will be located on the ship, as part of the DOE PARSL package.  At least one uplooking airborne lidar is planned, but the participation of a research-quality high-altitude downlooking lidar is not certain yet.  TWP-ICE will acquire microphysical profiles of cold tropical cirrus collocated with either CALIPSO overpasses or with ship-borne uplooking lidar, necessary to validate retrievals of extinction profiles in deep tropical ice clouds.  Additional validation opportunities are hoped to be provided by the participation of CPL in the field experiment. (http://science.arm.gov/~mather/darwiniop/)

 

Saharan Mineral dust experiment (SAMUM): SAMUM is designed to better understand the radiative effects of Saharan dust. The field campaign consists of aircraft, balloon, and ground-based instruments with numerical modeling activities. The project plans to begin operations in 2005. (http:// /www.tropos.de/samum).

 

Megacity Impacts on Regional and Global Environments (MIRAGE):  The goal of MIRAGE is to better characterize the chemical and physical transformations and fate of pollutants exported from large urban areas and to assess the impact of these pollutants on regional and global air quality, ecosystems and climate.. The mission is primary sponsored by NSF and will be formed around the deployment NCAR’s C-130 aircaft in the region surrounding Mexico City. The field experiment is planned for March 2006. (http://mirage-mex.ace.ucar.edu/index.html)

 

Cirrus Cloud Experiment (CIRCLE2): The CIRCLE experiment led by DLR seeks added information on the formation of mid-latitude cirrus and how aerosols can affect cirrus microphysical properties. The field campaign is planned in the autumn of 2006 in southern France and will seek to understand cloud-radiation interaction. Plans are to have both the DLR Falcon and the French Falcon to fly above ground-based measurement facilities (e.g., Observatoire de Haute-Provence).

 

African Monsoon Multidisciplinary Analyses (AMMA):  An international field mission is planned to improve our understanding of the West African monsoon. Specific areas of interest include how each of the following influence or are influenced by the monsoon circulation atmospheric dynamics, continental water cycle, atmospheric chemistry, continental and oceanic surface conditions. This mission involves field experiments coupled with satellite observations and modeling at different temporal and spatial scales. Four special observing periods are planned:  the first is scheduled for January-February 2006 during the dry phase, when dust and biomass burning aerosols co-exist and the others during the wet phase (late spring and summer 2006). Observations include balloon atmospheric soundings, airborne measurements with the new French ATR and Falcon 20, ground-based and oceanic measurements. CALIPSO validation flights are under consideration during the dry and the wet season. (http://www.joss.ucar.edu/amma/)

 

Arctic Study of Tropospheric Aerosol, clouds, and Radiation (ASTAR) and Antarctic trace Gas and Aerosol airborne Measurement Study (AGAMES).  ASTAR and AGAMES field missions are being led by the Alfred Wegener Institute for Polar and Marine Research (Germany) and consist of airborne field missions. AGAMES is planned for December 2005 through January 2006 and will be based from Antarctic stations at Neumayer and Syowa. The mission consists of 2 aircraft with one having a payload focused on aerosol observations. ASTAR is planned for March 2006 and will be based from Longyearbeyen, Spitsbergen. The airborne aerosol payload for both missions is expected to include a single channel, polarization sensitive lidar, particle samplers, a sun photometer (spanning 350-1050 nm), nephelometers, and radiometers.

 

Canadian Validation Support for CloudSat/CALIPSO. The Canadian Space Agency will sponsor intensive aircraft comparison activities tailored to the validation of mid and high latitude cloud systems primarily during the cold weather season.  Activities are scheduled for January-April 2006 The effort will include airborne flights with the NRC Convair 580 with in situ and remote sensing instruments (lidar/radar). Additional airborne flights with a Cessna 207 aircraft are also possible for summer months (lidar). These activities will be coordinated with other ground-based and mobile research facilities to optimize correlative measurements opportunities and scientific analysis.

 

Stratosphere-Climate Links with emphasis on the UTLS (SCOUT-O3). The European Union is sponsoring a major research initiative with studies covering ozone depletion and climate change, upper troposphere and lower stratosphere composition and transport processes, satellite validation, modeling activities. One aspect of the program is obtaining measurements in the UT/LS in tropical regions. Plans are now being considered for aircraft observations in the Darwin region for late 2005. The campaign would include the M-55 Geophysica and DLR Falcon 20. Both aircraft would support primarily in situ observations of aerosol and trace gases. Plans are being considered for balloon measurements in collaboration with AMMA in 2006. They would include an array of in situ and remote sensing trace gas and aerosol instruments. 

 

3.3.2 Ground-based Measurements

An important activity for CALIPSO validation is to link its measurements with those from established ground-based instruments over the globe. These are being organized under the CALIPSO Quid Pro Quo (QPQ) Validation Program. Comparisons between these data sets will permit an understanding of relative biases and place satellite measurements within the context of published observational records. Integrating measurements between different platforms also permits the formation of synergistic data sets that can explore complex multi-faceted physical processes. For example, the fusion of observations will particularly be valuable for better understanding the magnitude of the anthropogenic signal of aerosol forcing, for only with the combination of satellite, in situ, and modeling resources does sufficient information exist on the extensive and intensive properties of aerosols and the partitioning between natural and anthropogenic sources to address this issue.

 

A large number of ground-based instrument facilities make routine observations and can provide valuable correlative measurements for CALIPSO validation and collaborative science investigations. In general, the location of these facilities is somewhat scattered over the globe, but biased towards northern mid latitudes. Because CALIPSO will be in a high inclined orbit and tied to the WRS grid, the frequency of near coincident measurement opportunities with CALIPSO will be better at high latitude sites where orbits converge near the pole and poorer at low latitudes where the separation between orbits is greatest. Since clouds have high spatial and temporal variability relative to aerosols, correlative measurements for clouds (especially near active convection or near the boundary layer) require a greater degree of coincidence than for aerosols.  A statistical approach can be used where validated long-term surface measurements (such as at ARM sites) are compared statistically with regional satellite measurements.

 

A brief summary of ground-based networks that may support CALIPSO validation is provided below. Some of these sites such as those at Ny-Ålesund, Palaiseau, and the ARM sites and have been identified as being key validation locations. Dr. Tom Kovacs at Hampton University will lead coordination of these on-going measurement activities with CALIPSO over flight opportunities on a Quid Pro Quo (QPQ) basis. Details on this effort are described at the QPQ website (http://calipsovalidation.hamptonu.edu).

 

The Aerosol Robotic Network (Aeronet): The Aeronet is a federated network, with over 60 sites distributed over the globe, of sun photometers for the derivation of aerosol parameters (aerosol optical depth, inferred size distribution, refractive index, and phase function). (http://aeronet.gsfc.nasa.gov:8080/)

 

Asian Dust Network (AD-NET): The AD-Net is an international virtual community begun in February 2001 for the rapid notification and exchange of data of Asian dust events. (http://info.nies.go.jp:8094/kosapub/index.html).

 

Atmospheric Radiation Measurement (ARM) Program: Three highly instrumented facilities (Climate and Radiation Test Beds or CART) sites have been developed by the Department of Energy for measuring radiative energy flux profiles for clear and cloudy conditions. Sites are located at Southern Great Plains site in Oklahoma, the north shore of Alaska, and the Tropical Western Pacific. (http://www.arm.gov/). An HSRL system will be installed at the north shore site. A Raman lidar has been operational at the Southern Great Plains site for more than 5 years. The TWP will be a focus of study during the CRYSTAL-TWP program in 2005. The ARM sites are considered key validation sites for CALIPSO.

 

Baseline Surface Radiation Network (BSRN):  BSRN is a project of the World Climate Research Program (WCRP) aimed at detecting important changes in the earth's radiation field, which may cause climate changes. The BSRN provides observations of the short and longwave surface radiation flux. These readings are taken from a small number of selected stations, in contrasting climatic zones, together with collocated surface and upper air meteorological data and other supporting observations. (http://bsrn.ethz.ch/).

 

Canadian Research Facilities: The Canadian Space Agency will sponsor an extensive correlative measurement program for the CloudSat satellite experiment beginning in the summer of 2005.  at several sites to determine the dependencies of cloud characteristics by season. Ground-based lidar and radar measurements will be available from the CARE and King Radar facilities near Toronto, Canada. These will be complemented with new measurement systems that will be deployed at the Eureka research station beginning in 2006.

 

Climate Monitoring and Diagnostics Laboratory (CMDL):  The CMDL of the National Oceanic and Atmospheric Administration (NOAA) conducts research related to the atmospheric constituents that are capable of forcing change in the climate of the earth or may deplete the ozone layer. Aerosol measurements began at the CMDL baseline observatories in the mid-1970s as part of the Geophysical Monitoring for Climate Change. The goal of this regional-scale monitoring program is to characterize means, variability, and trends of climate-forcing properties of different types of aerosols, and to understand the factors that control these properties. (http://www.cmdl.noaa.gov/aerosol/)

 

European Aerosol Research Lidar Network (EARLINET):  EARLINET is a network of 22 ground-based lidar stations. Many of these facilities have additional remote sensing sensors that provide added information on aerosol properties.  The program was funded until 2003 by European Union and now operates on a voluntary basis (http://lidarb.dkrz.de/earlinet/index.html).

 

Micropulse Lidar Network (MPLNET):  MPLNET is a worldwide network of micro-pulse, autonomous single-channel (532 nm) lidar systems. The network is designed to provide long-term data sets of cloud and aerosol vertical distributions at key sites around the globe, and also serve as ground-truth sites for satellite measurement programs. MLPNET sites are co-located with AERONET sun photometers. (http://mplnet.gsfc.nasa.gov/).  The combined instrument facility located at the Chesapeake Lighthouse is of considerable interest because of its use in previous satellite validation campaigns and possible reference site for aircraft activities during early stages of the validation effort.

 

Network for the Detection of Stratospheric Change (NDSC): This network includes ~60 ground-based stations worldwide and a few mobile instruments, aimed at high-quality remote sensing of stratospheric composition and its changes over time. (http://www.ndsc.ws).

 

Observatoire de Physique de l’Atmosphere de La Reunion (OPAR): The OPAR station is located on Reunion Island in the Southern hemisphere and supports a two-channel backscatter lidar (532 and 1064 nm) with depolarization at 532 nm for cloud and aerosol studies. Measurements will be very useful for characterizing tropical cirrus clouds and tropospheric aerosols from biomass burning and in background conditions.

 

The Regional East Atmospheric Lidar Mesonet (REALM): REALM is a confederation of operational and planned lidar sites in eastern North America. The group includes elastic backscatter and Raman lidar systems with complementary aerosol and cloud remote sensing instruments.

 

Site Instrumental de Recherche par Télédétection Atmosphérique (SIRTA):  SIRTA is a comprehensive aerosol and cloud measurement facility supported IPSL that includes a backscatter multi-channel, depolation aerosol/cloud lidar, a water vapor Raman lidar, a 94 GHz radar, solar photometers, and radiometers located at Palaiseau, France. Observations from this site will provide important correlative measurements for validation and collaborative science studies. Past and future measurements provide valuable support for the development of synergistic retrievals of cloud and aerosol properties from A-train instruments. (http://sirta.lmd.polytechnique.fr/index_english.htm).

 

Surface Radiation Budget Network (SURFRAD):  SURFRAD was established in 1993 through the support of NOAA's Office of Global Programs. The SURFRAD mission's primary objective is to support climate research with accurate, continuous, long-term measurements of the surface radiation budget over the United States. This differs from the ARM/SGP site, where surface radiation budget measurements are also being made, in that ARM uses clustered measurements over a limited area for process-oriented studies. SurfRad sites are selected to represent diverse climates with homogeneous terrain. (http://www.srrb.noaa.gov/surfrad/surfpage.htm).

 

Mobile Remote Sensing Stations: Both Canadian and French research organizations are supporting the deployment of mobile remote sensing laboratories to provide direct comparisons of aerosol and cloud layer structures for CALIPSO. The TreSS (Transportable Remote Sensing Station) and LESAA mobile stations are sponsored by CNES and CNRS and will provide profile information on backscatter and extinction coefficients as well as information on the effects of multiple scattering. The TreSS facility will consist of a multi-channel mini-lidar, an IR radiometer (9.5-11.5 um), a pyranometer, and a 4-channel sun photometer. It is envisioned that the mobile laboratories would collect measurements primarily in -France during 2005, and possibly in northern Africa in 2006.  CSA is also sponsoring the Rapid Acquisition Scanning Aerosol Lidar (RASCAL) mobile facility, which includes a zenith pointing scanning lidar operating at 1064 and 532 nm. This facility would begin operation in the summer of 2005 in western Canada.

 

3.3.3 Satellite Comparisons

Comparisons with other satellite measurements will permit an assessment of relative biases of different data products between sensors for a variety of aerosol and/or cloud scenes over the globe. These studies may also provide insight into the spatial and temporal coherence of features detected by CALIPSO. Table 5 provides a partial listing of satellite observations that are expected to be available during the CALIPSO mission. Care must be exercised to ensure that products have similar sampling volumes and scenes are clearly understood before they are used for comparisons.

 


 

 

 

Table 5. Satellite Comparison DataSets

 

Instrument

Spacecraft

Measurement

AIRS

Aqua

Reconstruction of IIR filtered radiances

ASTER

Aqua

High spatial resolution surface emissivity

CERES

Aqua/Terra

Long-term stability (window 8-12 mm)

CloudSat

CloudSat

t, cloud heights

GLAS

ICESAT

t, sa(z), aerosol/cloud heights

MISR

Terra

t, index of refraction

MODIS

Aqua/ Terra

t, cloud fraction, cirrus particle size, emissivity, radiance

OMI

Aura

ta(z), aerosol index

PARASOL

PARASOL

t, aerosol index, cloud particle phase

SAGE III

Meteor 3M

Stratospheric t, sa(z)

SEVIRI

MSG

Radiance measurements, evaluate temporal sampling errors

 

3.3.4 Data Assimilation and Models

Combination of data from active and passive sensors on A-train satellites with operational ground-based instruments offers an unprecedented opportunity to better understand the effects of aerosols and clouds on climate and weather. Fusing these multiple data sources, however, is not straightforward because of inherent differences in measurement techniques and retrieval assumptions. Advanced data assimilation techniques and three-dimensional model simulations offer considerable promise for blending these resources and exploiting their full potential. It is hoped that through these tools insight into subtle correlations of between atmospheric parameters will be illuminated and better understood. The CALIPSO mission will seek to engage different assimilation and modeling groups for their support in CALIPSO validation and science studies.

 

3.4 Data Access Policy

 

Access to data acquired during CALIPSO validation activities will be in accordance with NASA’s data and information policy.

 

3.5 Data Ingest and Display Tools

 

The CALIPSO project is producing data ingest software for all of its Level 1 and 2 products that will be made available at the ATSC and the CALIPSO website (http:/www-calipso.larc.nasa.gov/.  The software code will be prepared in IDL and MATLAB.

 

To support data comparisons, satellite predict information will also be made available at the CALIPSO website. This information will be updated on a bi-weekly basis.

 

 


4. IMPLEMENTATION SCHEDULE

4.1 Data Release Requirements

 

The validation schedule outlined below is designed to support the verification and release of data products in three phases. The first phase is designed to support a preliminary or Beta release approximately 135 days after launch. This data set will include Level 1 products and a subset of Level 2 science data products as listed in Table 6. The second phase will support the release of validated Level 1 and 2 data products approximately 18 months after launch (see Table 1 or the Data Catalogue (PC-SCI-503) for an expanded description). The third phase will continue instrument and data product assessment studies to support a final report at the end of the mission Appropriate documentation describing the current assessment of the data products will accompany each data release. Publications on data quality will also be submitted to refereed journals. A comprehensive validation report of the entire data set will be prepared after the completion of the planned 3-year mission.

 

 

Table 6. Preliminary (Beta) CALIPSO science data release.

 

Data

Level

 

Data Products

 

Production Schedule

1

·   Calibrated lidar profiles

·   Calibrated IIR radiances

·   Calibrated WFC radiances

·   Meteorological profiles

·   Lidar aerosol & cloud browse images

Preliminary (Beta) release following on-orbit checkout (L+135 days).  Data produced on 2-day lag thereafter.

2

·   Aerosol layer height/thickness

·   Cloud height/thickness

Preliminary (Beta) release following on-orbit checkout (L+135 days). Data produced on 3-day lag thereafter.

 

 

 

4.2 Satellite Assessment Phase (L+0 to L+40 days)

 

The initial 40-day period following launch is designated as the Satellite Assessment Phase. During this period the satellite will be maneuvered into formation with Aqua; platform and payload systems will be activated and characterized. Under the nominal Assessment Phase schedule, instruments will be activated ~7 days after launch and begin checkout activities. An In-flight Acceptance Review will signal the transition to routine satellite operations.

 

 

 

 

 

4.3 Initial Instrument Validation (L+40 days to L+135 days)

 

Routine science operations are scheduled to begin approximately 40 days after launch. During the first few months of the mission, the Project team will focus mainly on internal assessments of the instrument performance and calibration activities.  For the lidar, initial analysis will include evaluation of laser energy, pointing and timing accuracy, stability of system constants, estimation of signal-to-noise ratios (day/night), and clear air depolarization. For the IIR and WFC, initial analysis will focus on pixel geolocation accuracy, image quality assessment, dark current and gain assessment, and internal calibration activities.  Examination of Quality Assurance (QA) reports generated as part of the routine data stream will be especially useful for identifying trends and deviations from expected behavior of Level 1 and 2 data handling routines and retrieval algorithms (see the CALIOP QA, WFC QA, and the IIR Level -1 documentation for details). 

 

During this early phase, several mission specific correlative measurement efforts are being organized and sponsored by NASA and CNES to aid assessment activities with external comparisons.  Within the first week of operation, a couple of flights with the NASA’s HSRL on board a chartered LearJet are planned along the spacecraft’s ground-track. These measurements should provide early feedback on altitude registration and overall instrument performance. More comprehensive analysis will be gained from a series of planned activities targeted at differing aerosol and cloud scenes during July – September.  To support aerosol validation, NASA LaRC’s HSRL and the NASA Ames’ Airborne Tracking Sunphotomer (AATS) instrument are planned to under fly CALIPSO along the east coast of the United States where aerosol loading is usually high during this period. The missions will be conducted over both land and water and during day and night (HSRL only). HSRL and AATS-14 will be deployed on separate aircraft. The combination of measurements will provide a degree of closure for determining CALIPSO’s measurement uncertainties. Flight opportunities will be planned with consideration of obtaining comparisons with MPL/Aeronet sites (e.g., Chesapeake Lighthouse Instrument Facility) and different aerosol types.   Approximately 10 flights are planned to verify altitude registration, to examine the sensitivity of the aerosol/cloud Feature Finder (under different scene compositions), and assess the accuracy of the retrieved data products under day and night conditions and with different aerosol mixtures. Flight opportunities will also be conducted over France in July/August and towards the end of September to evaluate the instrument performance of CALIOP and IIR. These activities will be led by IPSL and will include the deployment of several instruments that have similar instrument characteristics as the IIR (i.e., DIRAC, CLIMAT IR radiometer) with the LNG on the French Falcon aircraft in this first assessment phase. The deployment of the combined radar/lidar (LNG) RALI and CLIMAT systems is planned during the second assessment phase. These operations will be based near Paris.

 

It is further hoped that flight comparison opportunities will exist during the TCSP mission with CALIPSO. Obtaining correlative measurements of CPL attenuated backscatter at both 532 and 1064 nm over optically thick cirrus is extremely important for the mission. These measurements will be helpful for verifying whether spectral dependence between the two wavelengths is uniform; thereby, permitting the transfer of the calibration from CALIPSO’s 532 nm channel to its 1064 nm channel. Measurements of cloud extinction are also need to evaluate the a priori selection of Sc and corrections for multiple scattering. Simultaneous observations with MAS over clear ocean scenes will provide cross-reference measurements for IIR calibration analysis. Having direct comparisons between aircraft and CALIPSO is highly desirable and, if they do not occur because of a delayed launch, provisions should be made to obtaining these observations. Nevertheless, statistics acquired by CPL, MAS, and the other instruments will still provide meaningful guidance on the spectral dependence of cloud backscatter measurements and input assumptions. To add to these data sets, ground-based mobile lidar facilities sponsored by CNRS and CSA will also begin collecting overpass observations in July and August 2005.

 

During the first verification phase, comparisons with satellite observations from SAGE II/III will be conducted to verify the magnitude of aerosol extinction in the 30-34 km region, which is used for calibration of the 532 nm channel. These extinction profile measurements will provide one of the first comparison dataset of CALIOP level 2 products in the lower stratosphere where Sa is fairly well-known. Comparisons between IIR and WFC radiances will be intercompared to examine measurement consistency between instruments. These datasets will also be compared against climatological statistics complied from MODIS observations. As time permits, comparisons between concurrent MODIS (aerosol/cloud) and IIR/WFC/lidar products will be conducted.

 

Comparison opportunities will also be initiated with the QPQ team soon after the payload begins routine operations.  Because of limited coincidences, first comparison activities will be made with reference to climatological records from different sites. As the size of the data set increases (especially in the second phase), comparisons will be made by individual QPQ teams and findings communicated with the CALIPSO Algorithm Team.

 

A workshop will be held with the CALIPSO Science Team to review the quality of data products and changes to the data handling procedures and retrieval algorithms prior to the initial release of data at L+135 days. Tentative plans based on a June 17, 2005 launch readiness date are to hold this meeting in October 2005.

                       

4. Primary Validation Phase (L+135 to L+18 months)

           

The primary validation phase will occur from L+135 days until L+18 months. A sufficient number of measurements must be acquired and comparison activities completed to support the release of all CALIPSO products at L+18 months. Comparisons will be made with correlative measurements acquired from existing ground-based measurement programs on a Quid Pro Quo basis. Coordination of this effort is being led by Dr. Tom Kovacs at Hampton University, who will provide information to potential collaborators on measurement needs for CALIPSO validation and correlative observational opportunities. This effort will also include development of a web-based resource to catalogue and inform CALIPSO team members of available comparison data sets. The CALIPSO QPQ website is http://calipsovalidation.hamptonu.edu.

 

A number of complementary field campaigns are also being planned during this phase. A brief list is provided in section 3.3.1. These campaigns will include the coordinated deployment of aircraft, balloon, and ground-based platforms to address scientific questions concerning key issues in atmospheric chemistry, radiation and dynamics. Because many measurements collected during these campaigns will be of considerable value to CALIPSO validation concerns, and conversely as spaceborne measurements are expected to bring valuable complementary contributions, representatives from the science team will actively seek collaboration and support from the different field campaign management teams.

 

Data comparisons will be conducted by the CALIPSO science and algorithm teams and with collaborative measurement groups. A data comparison workshop is planned approximately 15 months after launch to support the major release of Level 2b products. Improvements to data handling procedures and algorithm retrievals are expected following this meeting. Revisions to the data sets will be archived at the Atmospheric Sciences Data Center at LaRC.

 

4.5 Continued Data Assessment Phase (post L+18 months)

 

Continued monitoring of CALIPSO instrument performance and data product quality will continue as products are regularly archived. Plans are to rely on QPQ data sets and inter-comparison opportunities available during different field measurement programs. Revised data sets will also be assessed and archived at the ASDC.

 

4.6 CALIPSO Validation Milestones (referenced to Launch Readiness Date)

 

Launch Readiness                                                                                             June 17, 2005

Initiate Payload Checkout Activities      (~ L+7 days )                                       June  2005

Initiate Laser, IIR, and WFC Instrument Operations      (~ L +40 days)             July 2005

TC4 Field Mission (Costa Rica)                                                                       July 2005

CALIPSO specific validation aircraft flights  (N. America)                           August 2005

CALIPSO specific validation aircraft flights (France)                                   August 2005)

CALIPSO specific validation aircraft flights (France)                                   September-October-2005)

Workshop on Level 1 Data Products                                                                (October 2005)           

Release Preliminary Level 1 Data Products (L+135 days)                                  October 2005

TWP-ICE Field Mission                                                                                  January-February 2006

AGAMES-ASTAR Field Mission                                                                     January-March 2006

AMMA Field Mission                                                                                      January-August 2006

CIRCLE2 Field Mission                                                                                  September 2006

Workshop on Comprehensive Data Comparison (L+15 months)                       October 2006

Release of Validated Level 1 and 2 Data Products (L+18 months)                     December 2006

 

 

5. MANAGEMENT

 

The CALIPSO Principal Investigator is responsible for the oversight of the mission and validation of the CALIPSO Science Data Products. The validation effort includes activities by the CALIPSO Science Team, Project engineers and algorithm development teams and Correlative Measurement investigators. Activities for assessing the performance of the CALIOP and WFC instruments will be conducted primarily by the combined mission operations, project, and science staff at NASA LaRC.  The performance assessment for the IIR and the validation of its Level 1 products is the responsibility of CNES, through the Technical Expertise Center located in Toulouse, France. Level 2 IIR validation activities are under the responsibility of IPSL. They will be conducted by IPSL, LAMP and LOA with the support of the ICARE Center in Lille, France.  Findings from the validation activities will be used to improve the retrieval algorithms and to verify error estimates. The results will be reported at scientific conferences and published in refereed journals.

 

To aid in the management of these validation activities, Dr. Chip Trepte will serve as the validation coordinator for US led measurement activities and Dr. Anne Garnier will serve as the validation coordinator for French and other European validation activities. Dr. Tom Kovacs will serve as the primary coordinator of measurement opportunities from existing instrument facilities on a quid pro quo basis. This validation team will also coordinate with CloudSat and other A-Train investigator teams and will seek advice from the ICESAT validation team on techniques and data sets that were profitable in its validation program. 

 

For these activities, the science and validation teams will be organized into working groups and will communicate via email, web links, and telecoms.  A data workshop is planned towards the end of the initial assessment period (nominally October 2005). The meeting will be open to external correlative measurement teams.

 

 

 

6. Contact Information

 

Dave Winker, PI                                                                                  David.M.Winker@nasa.gov

Jacques Pelon, Co-PI                                                                           Jacques.Pelon@aero.jussieu.fr

Pat McCormick, Co-PI                                                                        Pat.McCormick@hamptonu.edu

Chip Trepte, US Validation Coordinator                                               Charles.R.Trepte@nasa.gov

Anne Garnier, French Validation Coordinator                            Anne.Garnier@aerov.jussieu.fr

Tom Kovacs, QPQ Coordinator                                                           Tom.Kovacs@hamptonu.edu

 

CALIPSO Website                                                                              http://www-calipso.larc.nasa.gov/

CALIPSO QPQ Validation Website                                                     http://calipsovalidation.hamptonu.edu/