The document discusses strategies for optimizing data collection for the proposed GEO-CAPE mission through intelligent observation studies conducted by NASA's Goddard Space Flight Center team. Key findings include developing an observation operations simulator to examine different instrument and scheduling options, identifying cloud detection algorithms including the value of shortwave infrared bands, and establishing the feasibility of approaches like onboard cloud detection to reduce data handling costs. The simulator could be used to test different "what if" scenarios incorporating actual cloud forecast data and characterize instruments based on scene footprints. Possible future work involves integrating a scheduler with the simulator for live simulations, updating the tool with user feedback, and further analyzing instruments and cloud detection capabilities.
Long-term outdoor localisation with battery-powered devices remains an unsolved challenge,mainly due to the high energy consumption of GPS modules. The use of inertial sensors and short-range radio can reduce reliance on GPS to prolong the operational lifetime of tracking devices, butthey only provide coarse-grained control over GPS activity. An alternative yet promising approach is touse context-sensitive mobility models to guide scheduling and sampling decisions in localisationalgorithms. In this talk, I will present our work towards continental-scale long-term tracking of flyingfoxes, as part of the National Flying Fox Monitoring Program in Australia, using a model-drivenapproach. At the core of our approach is the multimodal GPS-enabled Camazotz sensor node platformthat has been designed at CSIRO for flying fox collars, with a cumulative weight just under 30g. The project has already deployed tens of devices on live flying foxes, which have been operating in thefield for several months. We are using the data from these devices to build mobility models andalgorithms for designing the next generation of software, as we will progressively deploy more than1000 nodes within the coming months. The progressive deployment of nodes coupled with delaytolerance, constrained resources, and incremental feature development raises interesting systemschallenges and opportunities, which I will highlight. The talk will also provide a snapshot of thecurrent data collection effort, and draw lessons from our activities in this area over the past 18 months
Long-term outdoor localisation with battery-powered devices remains an unsolved challenge,mainly due to the high energy consumption of GPS modules. The use of inertial sensors and short-range radio can reduce reliance on GPS to prolong the operational lifetime of tracking devices, butthey only provide coarse-grained control over GPS activity. An alternative yet promising approach is touse context-sensitive mobility models to guide scheduling and sampling decisions in localisationalgorithms. In this talk, I will present our work towards continental-scale long-term tracking of flyingfoxes, as part of the National Flying Fox Monitoring Program in Australia, using a model-drivenapproach. At the core of our approach is the multimodal GPS-enabled Camazotz sensor node platformthat has been designed at CSIRO for flying fox collars, with a cumulative weight just under 30g. The project has already deployed tens of devices on live flying foxes, which have been operating in thefield for several months. We are using the data from these devices to build mobility models andalgorithms for designing the next generation of software, as we will progressively deploy more than1000 nodes within the coming months. The progressive deployment of nodes coupled with delaytolerance, constrained resources, and incremental feature development raises interesting systemschallenges and opportunities, which I will highlight. The talk will also provide a snapshot of thecurrent data collection effort, and draw lessons from our activities in this area over the past 18 months
Differential Global Positioning System (DGPS) is an enhancement to Global Positioning System that provides improved location accuracy, from the
15-meter nominal GPS accuracy to about 10 cm in case of the best implementations. Differential Global Positioning System (DGPS) is a method of providing differential corrections to a Global Positioning System (GPS) receiver in order to improve the accuracy of the navigation solution. DGPS corrections originate from a reference station at a known location. The receivers in these reference stations can estimate errors in the GPS because, unlike the general population of GPS receivers, they have an accurate knowledge of their position.
DGPS uses a network of fixed, ground-based reference stations to broadcast the difference between the positions indicated by the GPS (satellite) systems and the known fixed positions. These stations broadcast the difference between the measured satellite pseudoranges and actual (internally computed) pseudoranges, and receiver stations may correct their pseudoranges by the same amount. The digital correction signal is typically broadcast locally over ground-based transmitters of shorter range.
DSD-INT 2020 Radar rainfall estimation and nowcastingDeltares
Presentation by Ruben Imhoff, Xiaohan Li, Pieter Hazenberg, Deltares, at the Delft-FEWS International User Days 2020, during Delft Software Days - Edition 2020. Monday, 2 November 2020.
Earth Viewing Systems Satellite Sensor Project, for Professor DiNardo's Course.
The presentation was given on 14th May, 2009.
______________________________________
I realize that some of the graphics do not have their sources cited, but I did not make those slides, and the group members who made them did not remember their sources. So, please forgive this oversight, since I consider it important enough to students of the earth surveillance class at The City College of New York (and elsewhere) that old presentations be available to them.
If, however, you can give me the sources of the graphics that you see, then I will be grateful, and I will be happy to cite them.
May 2012
You will hear about a research program in persistent surveillance. To identify terrorist activity and behavior, Livermore researchers have developed a data-processing pipeline that combines graphics-based computer hardware and clever software to extract meaning from wide-area overhead surveillance video.
The 2016 Remote Sensing Field camp will take the form of two projects.
A low tech, low cost aerial photography project using visible spectrum UAV/Ultralight Aircraft mounted cameras as the sensor to demonstrate that relatively low tech, low cost solutions can achieve surprisingly good results when compared to more commercial systems.
A more high tech, high cost terrestrial LiDAR collect of a building or structure of historical or architectural significance.
The scope of a project will influence all other aspects of the project, including its cost, timing, quality and risk.
Space Situational Awareness Forum
Following another very successful conference in London in November 2014, Space Situational Awareness 2015 took place in Hyattsville, Maryland in May 2015, with over 60 SSA experts from all over the globe coming together to discuss the most pressing SSA challenges.
With increasing dependence on space-based services, the ability to protect space infrastructure has become essential to our society. Any shutdown of even a part of space infrastructures could have significant consequences for the well-functioning of economic activities and our citizens’ safety, and would impair the provision of emergency services.
However, space infrastructures are increasingly threatened by the risk of collision between spacecraft and more importantly, between spacecraft and space debris. As a matter of fact, space debris has become the most serious threat to the sustainability of certain space activities.
In order to mitigate the risk of collision it is necessary to identify and monitor satellites and space debris, catalogue their positions, and track their movements (trajectory) when a potential risk of collision has been identified, so that satellite operators can be alerted to move their satellites. This activity is known as space surveillance and tracking (SST), and is today mostly based on ground-based sensors such as telescopes and radars.
With a focus on solving the political issues but not ignoring the technical, Space Situational Awareness 2015 the leading gathering of dedicated SSA experts from the USA, Europe and beyond, to discuss and debate the business, political and technical challenges that lie ahead.
Take a look at our previous Space Situation Awareness event…
Who should attend Space Situational Awareness?
Space Situational Awareness 2015 is a community of experts from Government, Space Agencies, Satellite/Spacecraft Operators, Space Lawyers, Space Insurance providers and Defense who are looking to understand and predict the physical location of natural and manmade objects in orbit around the Earth, with the objective of avoiding collisions.
How can you get involved in Space Situational Awareness?
If you feel that you could add to the debate and discussion at Space Situational Awareness, we’d be delighted to hear from you. Please drop us a line on +44(0)7769157787 or email me at adam.plom@coriniumintelligence.com.
Remote sensing –Beyond images
Mexico 14-15 December 2013
The workshop was organized by CIMMYT Global Conservation Agriculture Program (GCAP) and funded by the Bill & Melinda Gates Foundation (BMGF), the Mexican Secretariat of Agriculture, Livestock, Rural Development, Fisheries and Food (SAGARPA), the International Maize and Wheat Improvement Center (CIMMYT), CGIAR Research Program on Maize, the Cereal System Initiative for South Asia (CSISA) and the Sustainable Modernization of the Traditional Agriculture (MasAgro)
Differential Global Positioning System (DGPS) is an enhancement to Global Positioning System that provides improved location accuracy, from the
15-meter nominal GPS accuracy to about 10 cm in case of the best implementations. Differential Global Positioning System (DGPS) is a method of providing differential corrections to a Global Positioning System (GPS) receiver in order to improve the accuracy of the navigation solution. DGPS corrections originate from a reference station at a known location. The receivers in these reference stations can estimate errors in the GPS because, unlike the general population of GPS receivers, they have an accurate knowledge of their position.
DGPS uses a network of fixed, ground-based reference stations to broadcast the difference between the positions indicated by the GPS (satellite) systems and the known fixed positions. These stations broadcast the difference between the measured satellite pseudoranges and actual (internally computed) pseudoranges, and receiver stations may correct their pseudoranges by the same amount. The digital correction signal is typically broadcast locally over ground-based transmitters of shorter range.
DSD-INT 2020 Radar rainfall estimation and nowcastingDeltares
Presentation by Ruben Imhoff, Xiaohan Li, Pieter Hazenberg, Deltares, at the Delft-FEWS International User Days 2020, during Delft Software Days - Edition 2020. Monday, 2 November 2020.
Earth Viewing Systems Satellite Sensor Project, for Professor DiNardo's Course.
The presentation was given on 14th May, 2009.
______________________________________
I realize that some of the graphics do not have their sources cited, but I did not make those slides, and the group members who made them did not remember their sources. So, please forgive this oversight, since I consider it important enough to students of the earth surveillance class at The City College of New York (and elsewhere) that old presentations be available to them.
If, however, you can give me the sources of the graphics that you see, then I will be grateful, and I will be happy to cite them.
May 2012
You will hear about a research program in persistent surveillance. To identify terrorist activity and behavior, Livermore researchers have developed a data-processing pipeline that combines graphics-based computer hardware and clever software to extract meaning from wide-area overhead surveillance video.
The 2016 Remote Sensing Field camp will take the form of two projects.
A low tech, low cost aerial photography project using visible spectrum UAV/Ultralight Aircraft mounted cameras as the sensor to demonstrate that relatively low tech, low cost solutions can achieve surprisingly good results when compared to more commercial systems.
A more high tech, high cost terrestrial LiDAR collect of a building or structure of historical or architectural significance.
The scope of a project will influence all other aspects of the project, including its cost, timing, quality and risk.
Space Situational Awareness Forum
Following another very successful conference in London in November 2014, Space Situational Awareness 2015 took place in Hyattsville, Maryland in May 2015, with over 60 SSA experts from all over the globe coming together to discuss the most pressing SSA challenges.
With increasing dependence on space-based services, the ability to protect space infrastructure has become essential to our society. Any shutdown of even a part of space infrastructures could have significant consequences for the well-functioning of economic activities and our citizens’ safety, and would impair the provision of emergency services.
However, space infrastructures are increasingly threatened by the risk of collision between spacecraft and more importantly, between spacecraft and space debris. As a matter of fact, space debris has become the most serious threat to the sustainability of certain space activities.
In order to mitigate the risk of collision it is necessary to identify and monitor satellites and space debris, catalogue their positions, and track their movements (trajectory) when a potential risk of collision has been identified, so that satellite operators can be alerted to move their satellites. This activity is known as space surveillance and tracking (SST), and is today mostly based on ground-based sensors such as telescopes and radars.
With a focus on solving the political issues but not ignoring the technical, Space Situational Awareness 2015 the leading gathering of dedicated SSA experts from the USA, Europe and beyond, to discuss and debate the business, political and technical challenges that lie ahead.
Take a look at our previous Space Situation Awareness event…
Who should attend Space Situational Awareness?
Space Situational Awareness 2015 is a community of experts from Government, Space Agencies, Satellite/Spacecraft Operators, Space Lawyers, Space Insurance providers and Defense who are looking to understand and predict the physical location of natural and manmade objects in orbit around the Earth, with the objective of avoiding collisions.
How can you get involved in Space Situational Awareness?
If you feel that you could add to the debate and discussion at Space Situational Awareness, we’d be delighted to hear from you. Please drop us a line on +44(0)7769157787 or email me at adam.plom@coriniumintelligence.com.
Remote sensing –Beyond images
Mexico 14-15 December 2013
The workshop was organized by CIMMYT Global Conservation Agriculture Program (GCAP) and funded by the Bill & Melinda Gates Foundation (BMGF), the Mexican Secretariat of Agriculture, Livestock, Rural Development, Fisheries and Food (SAGARPA), the International Maize and Wheat Improvement Center (CIMMYT), CGIAR Research Program on Maize, the Cereal System Initiative for South Asia (CSISA) and the Sustainable Modernization of the Traditional Agriculture (MasAgro)
LVTS - Image Resolution Monitor for Litho-MetrologyVladislav Kaplan
Significant challenges for various Critical Dimension (CD) measurement matching procedures are reaching a comparable complexity as result of negative effects of roughness on the features. Due to the constant trend of integrated circuit in features reduction, impact of roughness start to be more destructive for various sets of measurement algorithms. Commonly used attempts to increase magnification for pattern recognition in measurement mode could in turn detect higher deviation from predefined patterns and thus initiate shift in placement of measurement gate. The purpose of this paper is to discuss how to reduce measurement gate (MG) placement variation impact and filter acquired data using edge correlation approach. The essence of listed above approach is to create set of width correlation function represents particular feature under test and compare it to “golden” one as a mean of detection of uncorrelated scans, which in turn should be excluded from overall computation of matching results. We describe general approach for algorithm stepping and various techniques for judgment of measurement comparison validity. Presented approach also has particular interest in determination of specified tool performance for predefined pattern recognition feature as well as for pattern recognition algorithm robustness study - direct interest for manufacturer. Precise matching estimation as part of Round Robin (RR) routines creating possibility to work with restricted amount of data and perform quick reliable qualification procedures. This paper concentrated on practical approach and used both simulation and actual data measurements data before and after proposed optimization taken by various generation tools by Hitachi (S-8840, S-9300, S-9380) in production environment
DSD-SEA 2023 Global to local multi-hazard forecasting - YanDeltares
Presentation by Kun Yan (Deltares) at the Seminar Models and decision-making in the wake of climate uncertainties, during the Deltares Software Days South-East Asia 2023. Wednesday, 22 February 2023, Singapore.
In this deck from GTC 2019, Seongchan Kim, Ph.D. presents: How Deep Learning Could Predict Weather Events.
"How do meteorologists predict weather or weather events such as hurricanes, typhoons, and heavy rain? Predicting weather events were done based on supercomputer (HPC) simulations using numerical models such as WRF, UM, and MPAS. But recently, many deep learning-based researches have been showing various kinds of outstanding results. We'll introduce several case studies related to meteorological researches. We'll also describe how the meteorological tasks are different from general deep learning tasks, their detailed approaches, and their input data such as weather radar images and satellite images. We'll also cover typhoon detection and tracking, rainfall amount prediction, forecasting future cloud figure, and more."
Watch the video: https://wp.me/p3RLHQ-k2T
Learn more: http://en.kisti.re.kr/
and
https://www.nvidia.com/en-us/gtc/
Sign up for our insideHPC Newsletter: http://insidehpc.com/newsletter
Introducing GNSS/GPS backup as a service (GBaaS)ADVA
We’re empowering service providers to offer GPS/GNSS-backup-as-a-service (GBaaS) as part of their SLAs. Based on our aPNT+™ platform and leveraging a suite of technologies - including multi-band GNSS receivers and AI- and ML-based management software - GBaaS enables end users to address the vulnerabilities of satellite-based and in-network timing. Now there's a simple and flexible way to achieve the highest levels of synchronization resilience and assurance and meet new guidelines and standards for redundant PNT architectures.
A REST Level 5 API is critical to allow users to meet their goals, perform activities, share and comments on those stories as they develop. This is the next generation API based on user stories, activities and behaviors.
Professional air quality monitoring systems provide immediate, on-site data for analysis, compliance, and decision-making.
Monitor common gases, weather parameters, particulates.
DERIVATION OF MODIFIED BERNOULLI EQUATION WITH VISCOUS EFFECTS AND TERMINAL V...Wasswaderrick3
In this book, we use conservation of energy techniques on a fluid element to derive the Modified Bernoulli equation of flow with viscous or friction effects. We derive the general equation of flow/ velocity and then from this we derive the Pouiselle flow equation, the transition flow equation and the turbulent flow equation. In the situations where there are no viscous effects , the equation reduces to the Bernoulli equation. From experimental results, we are able to include other terms in the Bernoulli equation. We also look at cases where pressure gradients exist. We use the Modified Bernoulli equation to derive equations of flow rate for pipes of different cross sectional areas connected together. We also extend our techniques of energy conservation to a sphere falling in a viscous medium under the effect of gravity. We demonstrate Stokes equation of terminal velocity and turbulent flow equation. We look at a way of calculating the time taken for a body to fall in a viscous medium. We also look at the general equation of terminal velocity.
Earliest Galaxies in the JADES Origins Field: Luminosity Function and Cosmic ...Sérgio Sacani
We characterize the earliest galaxy population in the JADES Origins Field (JOF), the deepest
imaging field observed with JWST. We make use of the ancillary Hubble optical images (5 filters
spanning 0.4−0.9µm) and novel JWST images with 14 filters spanning 0.8−5µm, including 7 mediumband filters, and reaching total exposure times of up to 46 hours per filter. We combine all our data
at > 2.3µm to construct an ultradeep image, reaching as deep as ≈ 31.4 AB mag in the stack and
30.3-31.0 AB mag (5σ, r = 0.1” circular aperture) in individual filters. We measure photometric
redshifts and use robust selection criteria to identify a sample of eight galaxy candidates at redshifts
z = 11.5 − 15. These objects show compact half-light radii of R1/2 ∼ 50 − 200pc, stellar masses of
M⋆ ∼ 107−108M⊙, and star-formation rates of SFR ∼ 0.1−1 M⊙ yr−1
. Our search finds no candidates
at 15 < z < 20, placing upper limits at these redshifts. We develop a forward modeling approach to
infer the properties of the evolving luminosity function without binning in redshift or luminosity that
marginalizes over the photometric redshift uncertainty of our candidate galaxies and incorporates the
impact of non-detections. We find a z = 12 luminosity function in good agreement with prior results,
and that the luminosity function normalization and UV luminosity density decline by a factor of ∼ 2.5
from z = 12 to z = 14. We discuss the possible implications of our results in the context of theoretical
models for evolution of the dark matter halo mass function.
This presentation explores a brief idea about the structural and functional attributes of nucleotides, the structure and function of genetic materials along with the impact of UV rays and pH upon them.
Phenomics assisted breeding in crop improvementIshaGoswami9
As the population is increasing and will reach about 9 billion upto 2050. Also due to climate change, it is difficult to meet the food requirement of such a large population. Facing the challenges presented by resource shortages, climate
change, and increasing global population, crop yield and quality need to be improved in a sustainable way over the coming decades. Genetic improvement by breeding is the best way to increase crop productivity. With the rapid progression of functional
genomics, an increasing number of crop genomes have been sequenced and dozens of genes influencing key agronomic traits have been identified. However, current genome sequence information has not been adequately exploited for understanding
the complex characteristics of multiple gene, owing to a lack of crop phenotypic data. Efficient, automatic, and accurate technologies and platforms that can capture phenotypic data that can
be linked to genomics information for crop improvement at all growth stages have become as important as genotyping. Thus,
high-throughput phenotyping has become the major bottleneck restricting crop breeding. Plant phenomics has been defined as the high-throughput, accurate acquisition and analysis of multi-dimensional phenotypes
during crop growing stages at the organism level, including the cell, tissue, organ, individual plant, plot, and field levels. With the rapid development of novel sensors, imaging technology,
and analysis methods, numerous infrastructure platforms have been developed for phenotyping.
Salas, V. (2024) "John of St. Thomas (Poinsot) on the Science of Sacred Theol...Studia Poinsotiana
I Introduction
II Subalternation and Theology
III Theology and Dogmatic Declarations
IV The Mixed Principles of Theology
V Virtual Revelation: The Unity of Theology
VI Theology as a Natural Science
VII Theology’s Certitude
VIII Conclusion
Notes
Bibliography
All the contents are fully attributable to the author, Doctor Victor Salas. Should you wish to get this text republished, get in touch with the author or the editorial committee of the Studia Poinsotiana. Insofar as possible, we will be happy to broker your contact.
What is greenhouse gasses and how many gasses are there to affect the Earth.moosaasad1975
What are greenhouse gasses how they affect the earth and its environment what is the future of the environment and earth how the weather and the climate effects.
Nutraceutical market, scope and growth: Herbal drug technologyLokesh Patil
As consumer awareness of health and wellness rises, the nutraceutical market—which includes goods like functional meals, drinks, and dietary supplements that provide health advantages beyond basic nutrition—is growing significantly. As healthcare expenses rise, the population ages, and people want natural and preventative health solutions more and more, this industry is increasing quickly. Further driving market expansion are product formulation innovations and the use of cutting-edge technology for customized nutrition. With its worldwide reach, the nutraceutical industry is expected to keep growing and provide significant chances for research and investment in a number of categories, including vitamins, minerals, probiotics, and herbal supplements.
Nutraceutical market, scope and growth: Herbal drug technology
GeoCAPE Strategies
1. 1
GEO-CAPE INTELLIGENT OBSERVATION
STUDIES @GSFC
Pat Cappelaere
GSFC Team: Stu Frye, Karen Moe,
Dan Mandl, Jacqueline LeMoigne,
Tom Flatley, Alessandro Geist
GEO-CAPE Workshop
September 1, 2015
http://geocape.herokuapp.com
2. 2
+ Forecasting
+ Sub-Gridding
+ Cloud Detection
+ Onboard
Detection
Algorithms
+ Architecture
+ Strategies
+ KISS
+ Schedule Layout
+ Visualization
+ Ground
Processing
+ Distribution
+ Next Steps
+ Backup Material
+ Open Questions
TABLE OF CONTENTS
+ Mission
+ Instruments
+ Selection
+ Scheduling
Assumptions Clouds Scheduling Closing
01 02 03 04INTRO
Summary
3. 3
STRATEGIES OVERVIEW
Strategy 1
Ground Scheduler
With Simple
Priorities
Potentially
Acquired Scenes
per hour
< 10 scenes
Complexity:
Cost:
Based On Current Assumptions That Need To Be Validated
Strategy 2
Ground Scheduler
With Cloud
Forecast
~ 14 scenes
Strategy 3
Ground Scheduler
With Sub-area
Forecast
~16 scenes
Strategy 4
Onboard
Scheduler and
Onboard Cloud
Detection
~ 19 scenes
Strategy 5
Smart Onboard
Scheduler and
onboard Image
Processing to
Reduce Downlink
Costs
~ 19.2 scenes
4. 4
OBJECTIVES OF GSFC STUDY ELEMENTS
Smart Cloud Forecasting
Analyze And Summarize Strategies To Improve Science Data Collection
Onboard Cloud Detection Ground/Onboard Scheduling
with Robust Executive
6. 6
MISSION ASSUMPTIONS
Mission Life Time: 5 years
~16 hours of Operations per
day
Survey Mode
U.S Coastal Waters: East
Coast, Gulf Coast, West Coast,
Puerto Rico, Great Lakes
Targeted Events As Necessary
Regions of Interests
Other Coastal Waters of North
& South America
Anywhere within Field of
Regard
Optimize Acquisition of “Cloud Free” Scenes At Lowest Cost
01
7. 7
MISSION ASSUMPTIONS 01
Optimize Acquisition of “Cloud Free” Scenes At Lowest Cost
Standard (Threshold) Survey
Mode (60min Repeat
Frequency)
High Repeat (Baseline) Mode
(30mn Repeat Frequency)
Targeted Events and Regions
of Special Interest
Engineering Tasks and Special
Window Events (Sun
interference…)
Some scenes will be requested
by external users and subject to
Science Team Approval
Scenes will need some kind of a
priority scheme for scheduling
8. 8
Instrument Type
Filter
Radiometer
FR
Filter
Radiometer
FR
Wide
Angle
Spectro-
meter
WAS
Multi-Slit
Spectro-
meter
COEDI
Multi-Slit
Spectro-
meter
COEDI
Spatial Resolution
(m) (nadir)
250 375 375 375 250
Spectral Resolution
(nm)
5 nm 5 nm 0.4 nm 0.4 nm 0.4 nm
Spectral Range (nm)
(2135 not req)
Multispectral
(50) 340-1050;
1245, 1640, 2135
Multispectral
(50) 340-1050;
1245, 1640, 2135
340-1050;
1245, 1640,
2135 nm
340-1050
1245,1640 nm
340-1050
1245,1640 nm
Scan Rate (km2/min) 100,105 100,105 48,200 43,200 28,800
Mass CBE (kg) 190.4 126.3 309.4 202.8 358.6
Power CBE (W) 200.1 161.2 341.3 192.5 257.7
Volume
(m x m x m)
1.5 x 1.46 x 1.02 1.0 x 0.97 x 0.68
2.6 x 1.8 x
1.5
1.5 x 1.7 x 1.1 2.2 x 2.5 x 1.7
Telemetry CBE
(kbps)
15,900 10,600 23,832 23,854 35,765
Detector Size 4k X 4K 2730 X 2730 8k X 1k 2k X 1k (x 2) 3k X 1k (x 2)
Real Detector Size 4096 x 4096
Line scanner
(8K)
2 line scans
2048
20 pixels apart
2 line scans
3072
20 pixels apart
INSTRUMENT CONCEPTS & CAPABILITY
9. 9
THRESHOLD FR ASSUMPTIONS @375M
• Detector Size 2730 x 2730
• Subsampled 2x2 – initial spatial
resolution 187.5m -> 375m final
• Scan Rate: 100,134 km2/min -> 157
seconds per scan
• Scan Rate:
2730*2730*0.1875*0.1875*60/157 =
100,134 km2/min
• Final Scene Size: 1365 x 1365 pixels
(512km x 512km)
• Total Time including mirror
displacement = 157s + 1s = 158s
• 50+3 bands ??? @ 2bytes/pixels
01
• Scene Size: 53*2*1365*1365 = 197.5 MB
• Data Ingest Rate: 197.5 / 158 = 1.250 MB/s
• Estimated Daily Storage/Downlink:
21 scenes/hr. * 16hr/day * 444.6MB = 65.7 GB
• Estimated Monthly Downlink: 1.97 TB
Example of Instrument
Analysis for each of 4 options
10. 10
Strawman 18 Coastal/Lakes Survey Scenes Using FR
01
Source: GSFC analysis via GUI Editor, assuming spherical Earth – Satellite at 95W
11. 11
INSTRUMENT ANALYSIS COMPARISON
11
FR FR COEDI WAS
Resolution 250m 375m 375m 375m
Scene Size 512 x 512 km 512 x 512km 768 x 535.5km 1536 x 375 km
Scene Storage 446.6MB 197.5 MB 304.15 MB 434.2 MB
High Repeat
Baseline (30min)
11 scenes 11 scenes 8 scenes 2 scenes
Threshold (1hr) 22 scenes 22 scenes 17 scenes 4 scenes
CONUS Coverage 18 scenes 18 scenes 15 scenes 13 scenes
Data Rate 2.814 MB/s 1.25 MB/s 1.46 MB/s 0.57 MB/s
Parametric Cost
($M)
$132M $108M 136.2M 165.2M
Daily
Storage/Downlin
k
150 GB 65.7 GB 102.2 GB 145.9 GB
Monthly
Downlink
4.5 TB 1.97 TB 3.1 TB 4.38 TB
01
13. 13
SURVEY SCENES & FORECAST 01
02
Example FR Scene
Forecast Schedule
Red scenes fail cloud
threshold and are
not scheduled
Green scenes pass
cloud threshold and
are scheduled
Orange scenes are
marginal and are
scheduled for more
evaluation onboard
14. 14
CLOUD THRESHOLDING STRATEGY
Two Cloud Thresholds: Green, Orange
- Below Green Threshold: Cloud Coverage is Acceptable For Science Team, Scene is
Green
- Above Orange, Scene Is Not Even Scheduled On the Ground, Scene is Red
- Between Green And Orange: Scene Can Be Scheduled, But Will Be Checked On
Board. It May Become Green
This Allows Higher Threshold Values For Use by Ground Scheduler
After Acquisition, Onboard Cloud Detection Is Used To Check Scene Against Green Thresholds.
Scenes Can Then Be Accepted or Rejected.
~ 20% Chance to Accept Marginal Scenes and increase Scene Marginal Return
~ 20% Chance to Reject Marginal Scenes and Optimize Data Downlink/Storage
The ~20% acceptance/rejection of marginal scenes is based on studies done for HyspIRI,
GEWEX and other analysis listed in the reference backup.
01
02
15. 15
GROUND CLOUD FORECAST SUB-GRIDDING
Cloud Forecast Optimization Strategy
Rationale: Focus Cloud Forecast on Sub-areas
of the Scene (sub-grids)
Forecast is obtained at the center of sub-area
of interest (and not on a pixel by pixel basis).
This is faster and cheaper.
Scene Forecast is then calculated by averaging
the forecasts of sub-areas.
01
02
16. 16
ONBOARD CLOUD DETECTION
Strategy to Resolve Orange (marginal) Scenes using Scene Sub-grids
Rationale: Determine if the orange scheduled
scenes were actually within the acceptable
green threshold for science quality in order to
make decisions about downlinking and
rescheduling
Approach: Evaluate only coastal zone sub-
grids (masking out sub-grids over land, for
example) and average those results to
determine if the green threshold is met; if
successful downlink those observations; if too
cloudy, delete to reduce downlink costs
01
02
17. 17
SPECTRAL BANDS USED FOR CLOUD DETECTION BY OTHER SENSORS
COMPARED TO THE BANDS AVAILABLE ON GEO-CAPE
Sentinel 2
Band number Central Bandwith (nm) Spatial resolution (m)
wavelength (nm)
1 443 20 60
2 490 65 10
3 560 35 10
4 665 30 10
5 705 15 20
6 740 15 20
7 783 20 20
8 842 115 10
8b 865 20 20
9 945 20 60
10 1380 30 60
11 1610 90 20
12 2190 180 20
12 bands
at different
resolutions
Notes:
- Thermal bands distinguish clouds from ice.
- SWIR band 1375nm (used by EO-1 / Landsat-
8 / Sentinel 2) is the most critical to detect
high cirrus clouds that contaminate scenes,
especially in Coastal Areas.
19. 19
USER SCENARIO TO SUBMIT NEW REQUESTS
• Science team members are provided user front end GUI to add/remove
scenes and edit scene attributes
• They enter scene parameters including location, size, priority, number of
collects, cloud coverage thresholds, etc…
• Requests are submitted and can be accepted or rejected by the scheduling
system. Every 6 hours the front end assembles the scenes to be imaged,
including engineering tasks and activity blackouts, and gathers the cloud
forecast for each scene
• The scenes are scheduled based on scene attributes and cloud forecasts. The
schedule may be reviewed by the science team and potentially rejected.
Scene attributes may have to be tweaked and ingested by the scheduling
system to generate a new plan
• Approved schedule is generated and uplinked after science team approval
01
02
03
24. 24
GeoSOCIAL
API
Full Access to Final
Product(s) &
MetaData
Easy To Share And
Distribute to
Community of
Interest
Realtime User
Notifications
01
02
03
04
BROWSE
SNAPSHOT
25. 25
Summary:
Key Findings
• GEO-CAPE Observation Operations Simulator developed
• Hosted Payload data handling and potential cost savings examined
• Candidate cloud detection algorithms identified, including value of SWIR band 1375nm
• Feasibility established for
• Cloud threshold settings and forecast constraints, incorporating marginal scene handling
• Onboard processing of cloud detection to not downlink marginal observations that fail cloud
threshold (reduce data handling costs)
• Cost of onboard processing capability with 2015 technology
Use GSFC Observation Ops Simulator Tool (http://geocape.herokuapp.com)
• Examine “What If” scenarios incorporating actual cloud forecast data for example/fixed targets
• Characterize instrument scene based on foot print center point to generate target observation
requests
Possible Follow-on Activities
• Integrate scheduler with simulator to enable live simulations with dynamic targets (1-2 month)
• Update Simulator tool per user feedback (days to weeks)
• Analyze VNIR Band Study for High Cloud Detection (1-2 months)
• Research Commercial Vendor Communication Capabilities, Cost & API (1-2 months)
01
02
03
04
28. 28
COMMERCIAL DOWNLINK COST (DOD)
Current Satellite Type AOR MHz Mbps Cost Cost per MHz Mbps to MHz
Conversion Ratio
IS-20 Ext Ku AFG 60 100 $200,000 $3,333 1.67
IS-17 Ku ME Inroutes 8.1 13.5 $27,000 $3,333 1.67
IS-17 Ku ME Outroutes 24.2 31.5 $63,000 $2,603 1.30
IS-17 C ME - Oman 36 64 $128,000 $3,556 1.78
This table reflects current DOD prices for Commercial Satellite
Access. NASA costs have been assumed to be comparable
01
02
03
04
SATELLITE INTERNET COST (IDIRECT)
Coverage CONUS
Source: http://www.groundcontrol.com/US_Canada_Satellite_Internet.htm
750GB/month, 40 sites $56K/month
$0.14 per MB
29. 29
LANDSAT-7 BANDS USED FOR CLOUD DETECTION
Band
Number
Wavelength
(Range)
Spatial Resolution
(in meters)
2 0.52-0.60 30
3 0.63-0.69 30
4 0.77-0.90 30
5 1.55-1.75 30
6 (Thermal IR) 10.40-12.50 60 (30 after 02/2010)
Landsat-8 Bands Used for Cloud Detection
Band
Number
Wavelength
(Range)
Spatial Resolution
(in meters)
3 0.53 - 0.59 30 m
4 0.64 – 0.67 30 m
5 0.85 – 0.88 30 m
6 1.57 – 1.65 30 m
9 1.36-1.38 30 m
10 10.60 – 11.19 100 m * (30 m)
11 11.50 – 12.51 100 m * (30m)
EO-1/Hyperion Bands Used for Cloud Detection
Band
Number
Wavelength
(Central)
Spatial Resolution
(in meters)
21 0.56 30
31 0.66 30
51 0.86 30
110 1.25 30
123 1.38 30
150 1.65 30
GOES Bands Used for Cloud Detection
Band
Number
Wavelength
(Range)
Spatial Resolution
(in kilometers)
2 3.8 – 4.0 4 km
4 10.2 – 11.2 4 km
5 11.5 – 12.5 4 km
6 12.9 – 13.7 4 km
* TIRS bands are acquired at 100 meter resolution, but
are resampled to 30 meter in delivered data product.
Band
Number
Wavelength
(Central)
Spatial Resolution
(in meters)
1 0.645 250 m
2 0.858 250 m
5 1.240 500 m
6 1.640 500 m
7 2.130 500 m
20 3.750 500 m
31 11.030 500 m
26 1.375 500 m
MODIS Bands Used for Cloud Detection
CLOUD DETECTION ALGORITHMS DETAILS
30. 30
REFERENCES (1 of 2)
References for Cloud Detection Algorithms: N. Memarsadeghi, “A Review of Landsat-7 and EO-1 Cloud Detection
Algorithms,” on the Imagepedia section of the IMAGESEER website,
https://imageseer.nasa.gov/imagepedia/Imagepedia_7_CloudDetection_Nargess_Jan2011.pdf
M. Griffin, H. Burke, D. Mandl, and J. Miller. “Cloud Cover Detection Algorithm for EO-1 Hyperion Imagery” in 2003 IEEE
International Geoscience and Remote Sensing Symposium (IGARSS), July 2003, vol. 1, pages: 86-89. Cloud Detection.
T. Doggett, R. Greeley, S. Chien, R. Castano, B. Cichy, A. G. Davies, G. Rabideau, R. Sherwood, D. Tran, V. Baker, J. Dohm,
and F. Ip, “Autonomous detection of cryospheric change with hyperion on-board Earth Observing-1”, Remote Sensing of
Environment, Vol. 101, Issue 4, April 2006, pages 447-462.
Doggett_et_al, Correspondences with Thomas Doggett, January-April, 2008.
Correspondences with Michael K. Griffin, MIT Lincoln Laboratory, August 2010.
EO-1 Website (http://eo1.gsfc.nasa.gov/), EO-1 Preliminary Technology and Science Validation Report,
http://eo1.gsfc.nasa.gov/new/validationReport/index.html#part14, and Cloud detection related publications and
presentations listed on above link under Part 7 (Sensor Web/ Test bed Initiatives, Section 5.
Hyperion cloud detection algorithm (General Overview):
http://eo1.gsfc.nasa.gov/new/validationReport/Technology/SensorWebs/Final%20Rpt_Appendix_Cloud%20Cover%20Val.
ppt
E. El-Araby, T. El-Ghazawi, J. Le Moigne, and R. Irish, “Reconfigurable Processing for Satellite On-Board Automatic Cloud
Cover Assessment (ACCA)”, Journal of Real Time Image Processing, 2009, Vol. 4, No. 3, pp. 245-259. Landsat-Cloud
Detection.
ACCA algorithm (General Overview): http://landsathandbook.gsfc.nasa.gov/pdfs/ACCA_slides.pdf
31. 31
REFERENCES (2 of 2)
Landsat Handbook (http://landsathandbook.gsfc.nasa.gov/), ACCA Algorithm:
http://landsathandbook.gsfc.nasa.gov/htmls/acca.html and http://landsathandbook.gsfc.nasa.gov/pdfs/ACCA_slides.pdf
Landsat facts: http://geo.arc.nasa.gov/sge/landsat/l7.html
G. Jedlovec, “Automated Detection of Clouds in Satellite Imagery”, in Advances in Geoscience and Remote Sensing, Edited by G. Jedlovec,
2009.
M.D. King et al, “Cloud Retrieval Algorithms for MODIS: Optical Thickness, Effective Particle Radius, and Thermodynamic Phase”,
MODIS Algorithm Theoretical Basis Document, 1997.
S. Ackerman et al (“Discriminating Clear-Sky from Cloud with MODIS,” MODIS Algorithm Theoretical Basis Document, 2010.
References for Cloud Predictions:
- Global Cloud Cover for Assessment of Optical Satellite Observations Opportunities: A HyspIRI Case Study, M. Mercury, R. Green,
et al Remote Sensing of Environment journal 126 (2012) 62-71
- Climatic Atlas of Clouds [http://www.atmos.washington.edu/CloudMap/]
- GEWEX Study: Assessment of Global Cloud Data Sets from Satellites [http://www.wcrp-
climate.org/documents/GEWEX_Cloud_Assessment_2012.pdf]
- Trends in Global Cloud Cover in Two Decades of HIRS Observations [http://journals.ametsoc.org/doi/pdf/10.1175/JCLI3461.1]
- Empirical experience from EO-1 tasking. Formal simulation may be required to firm up the threshold numbers
32. 32
How do short-term
coastal and open ocean
processes interact with and
influence larger scale
physical, biogeochemical
and ecosystem dynamics?
(OBB 1)
How are variations in
exchanges across the land-
ocean interface related to
changes within the
watershed, and how do
such exchanges influence
coastal and open ocean
biogeochemistry and
ecosystem dynamics?
(OBB 1 & 2; CCSP 1 & 3)
How are the
productivity and
biodiversity of coastal
ecosystems changing, and
how do these changes
relate to natural and
anthropogenic forcing,
including local to regional
impacts of climate
variability? (OBB 1, 2 & 3;
CCSP 1 & 3)
How do airborne-
derived fluxes from
precipitation, fog and
episodic events such as
fires, dust storms &
volcanoes affect the
ecology and
biogeochemistry of coastal
and open ocean
ecosystems? (OBB 1 & 2;
CCSP 1)
How do episodic
hazards, contaminant
loadings, and alterations of
habitats impact the biology
and ecology of the coastal
zone? (OBB 4)
Short-Term
Processes
Land-
Ocean
Exchange
Impacts of
Climate
Change &
Human
Activity
Impacts of
Airborne-
Derived
Fluxes
Episodic
Events &
Hazards
GEO-CAPE Oceans STM
Mapsto
Science
Question
GEO-CAPE Science Questions are traceable to NASA’s OBB Advanced Planning Document (OBB) and the U.S. Carbon Cycle Science Plan (CCSP).
Water-leaving radiances in
the near-UV, visible & NIR
for separating absorbing &
scattering constituents &
chlorophyll fluorescence
Product uncertainty TBD
Temporal Resolution:
Targeted Events:
• Threshold: ≤1 hour
• Baseline: ≤0.5 hour
Survey Coastal U.S.:
• Threshold: ≤3 hours
• Baseline: ≤1 hour
Regions of Special Interest
(RSI): Threshold: ≥1 RSI 3
scans/day
• Baseline: multiple RSI 3
scans/day
Other coastal and large
inland bodies of water
within ocean color FOR:
• Baseline: ≤3 hours
Spatial Resol. (nadir):
• Threshold: ≤375 x 375 m
• Baseline: ≤250 x 250 m
Field of Regard for Ocean
Color Retrievals:
60°N to 60°S;
155°W to 35°W
Coastal Coverage*:
width from coast to ocean:
• Threshold: min 375 km
• Baseline: min 500 km
Scanning Priority:
•Threshold:
1. U.S. Coastal Waters* 3
to 8 times per day
2. Other coastal and large
inland bodies of water
3. Open ocean waters
within FOR
5
1 2
4
GEO-CAPE will observe coastal regions at sufficient
temporal and spatial scales to resolve near-shore
processes, tides, coastal fronts, and eddies, and track
carbon pools and pollutants. Two complementary
operational modes will be employed:
(1) survey mode for evaluation of diurnal to
interannual variability of constituents, rate
measurements and hazards for estuarine and
continental shelf and slope regions with linkages to
open-ocean processes at appropriate spatial scales,
and (2) targeted, high-frequency sampling for
observing episodic events including evaluating the
effects of diurnal variability on upper ocean
constituents, assessing the rates of biological
processes and coastal hazards.
Measurement objectives for both modes include:
(a) Quantify dissolved and particulate carbon pools
and related rate measurements such as export
production, air-sea CO2 exchange, net community
production, respiration, and photochemical oxidation
of dissolved organic matter.
(b) Quantify phytoplankton properties: biomass,
pigments, functional groups (size/taxonomy/Harmful
Algal Blooms (HABs)), daily primary productivity using
bio-optical models, vertical migration, and chlorophyll
fluorescence.
(c) Measure the inherent optical properties of coastal
ecosystems: absorption and scattering of particles,
phytoplankton and detritus, CDOM absorption.
(d) Estimate upper ocean particle characteristics
including particle abundance and particle size
distribution.
(e) Detect, quantify and track hazards including HABs
and petroleum-derived hydrocarbons.
GEO-CAPE observations will be integrated with field
measurements, models and other satellite data:
(1) to derive coastal carbon budgets and determine
whether coastal ecosystems are sources or sinks of
carbon to the atmosphere,
(2) to quantify the responses of coastal ecosystems
and biogeochemical cycles to river discharge, land
use change, airborne-derived fluxes, hazards and
climate change, and
(3) to enhance management decisions with improved
information on the coastal ocean, such as required for
Integrated Ecosystem Assessment (IEA), protection of
water quality, and mitigation of harmful algal blooms,
oxygen minimum zones, and ocean acidification.
53
Spectral Range:
Hyperspectral UV-VIS-NIR
• Threshold: 345-1050 nm; 2 SWIR
bands 1245 & 1640 nm
• Baseline: 340-1100 nm; 3 SWIR
bands 1245, 1640, 2135 nm
•Spectral Sampling & Resolution:
• Threshold: UV-Vis-NIR: ≤2 & ≤5nm;
400-450nm: ≤0.4 & ≤0.8nm (for NO2
at spatial resolution of 750x750m at
nadir); SWIR resolution: ≤20-40 nm
• Baseline: UV-ViS-NIR: ≤0.25 & 0.75
nm; SWIR: ≤20-50 nm
Geostationary orbit
at 95W longitude to
permit sub-hourly
observations of
coastal waters
adjacent to the
continental U.S.,
North, Central and
South America
Storage (up to 1
day) and download
of full spatial data
and spectral data.
Western
hemisphere data
sets from models,
missions, or field
observations
Measurement
Requirements
(1) Ozone
(2) Total water
vapor
(3) Surface wind
velocity
(4) Surface
barometric
pressure
(5) Vicarious
calibration &
validation - coastal
(6) Full prelaunch
characterization
(7) Cloud cover
Science
Requirements
(1) SST
(2) SSH
(3) PAR
(4) UV solar
irradiance
(5) MLD
(6) Air/Sea pCO2
(7) pH
(8) Ocean
circulation
(9) Tidal & other
coastal currents
(10) Aerosol
deposition
(11) run-off
loading in coastal
zone
(12) Wet
deposition in
coastal zone
(13) Wave height
& surface wind
speed
Validation
Requirements
Conduct high
frequency field
measurements
and modeling to
validate GEO-
CAPE retrievals
from river mouths
to beyond the
edge of the
continental
margin.
Approach
Measurement
Requirements
Instrument
Requirements
Platform
Requirem.
Ancillary
Data
Requirem
Draft v.4.6 - Feb. 28, 2013
* Coastal coverage within field-of-view (FOV) includes major estuaries and rivers such as Chesapeake Bay, Lake Pontchartrain/Mississippi River delta and the Laurentian Great Lakes,
e.g., the Chesapeake Bay coverage region would span west to east from Washington D.C. to several hundred kilometers offshore (total width of 375 km threshold).
Signal-to-Noise Ratio (SNR) at Ltyp(70˚ SZA):
• Threshold: ≥1000 for 10 nm FWHM (350-800 nm);
≥600 for 40 nm FWHM (800-900 nm); ≥300 for 40 nm
FWHM (900-1050 nm); ≥250 and ≥180 for 1245 &
1640 nm (20 & 40 nm FWHM); ≥500 NO2 band.
• Baseline: ≥1500 for 10 nm (350-800 nm); NIR,
SWIR and NO2 bands same as threshold; ≥100 for
the 2135nm (50nm FWHM)
• Threshold: Aggregate SWIR bands to 2x2 GSD
pixels to meet SNR; Baseline: No aggregation.
Scanning area per unit time: Threshold: ≥25,000
km2/min; Baseline: ≥50,000 km2/min
Field of Regard:
• Full disk: 20.8° E-W and 19° N-S imaging
capability from nadir for Lunar & Solar Calibrations
Non-saturating detector array(s) at Lmax
On-board Calibration:
• Lunar: Threshold: minimum monthly;
Baseline: same as threshold
• Solar: Threshold: none; Baseline: daily
Polarization Sensitivity: <1.0%
Relative Radiometric Precision:
• Threshold: ≤1% through mission lifetime
• Baseline: ≤0.5% through mission lifetime
Mission lifetime: Threshold: 3 years; Goal: 5 years
Intelligent Payload Module Baseline only: Near Real-Time satellite data
download from other sensors (GOES, etc.) for on-board autonomous decision
making.
Pre-launch characterization: Adequate to achieve the required on-orbit
radiometric precision
Science
Questions
3
2
1
Science
Focus
5
4
2
3
3
5
1
2
4
1 2 4 53
1 2 3
1 2 4 53
1 2 3
Error (as % of nadir pixel) Threshol
d
Baselin
ePointing Knowledge LOS <50% <10%
Pointing Accuracy LOS <100% <25%
Pointing Stability LOS <50% <10%
Geolocation Reconstr. <100% <10%
1 2
4
5
3
Note: COEDI bundle is far greater that 150km noted from Antonio June 18, 2015
Regarding size of the COEDI scenes for STK analysis: assuming 75km width (5x15km) requires ~100 scenes. Can we use a larger width (10x15km)?
Sure
Red scenes will not be scheduled
Orange scenes will be scheduled
They will need to be green when acquired onboard (see discussion later)
- Forecast may not be as accurate further ahead
- Cloud detection could also be done at the sub-grid level
Green threshold would be used onboard to accept/reject scene
Difference could be ~20% either way (accepting more scenes or rejecting cloudy scenes)
High cirrus clouds may not be visible and can really contaminate a coastal zone scene. We need to be able to detect them onboard AND on the groundGrid size (px)
High repeat events could be guaranteed spacing (if not more than 10)
We could also schedule them first if spacing is not that important
Imaging start at sunrise/sunset for each target location (part of forecast data)
Forecast is generated for 24hrs
Schedule is generated every 6 hours 06:00, 12:00, 18:00 [, 24:00]
Admin user has 2 hours to replace it if not acceptable. Latest schedule is automatically uploaded every six hours at 08:00, 14:00, 20:00 [, 02:00]
Snapshot from website.
Only one day has been loaded/selected
Scenes can also be filtered by scene name, status (scheduled, complete, failed…) and date…
Ground could request a scene retransmit
Ground could manage recorder and delete received scenes