Artificial intelligence (AI) is experiencing steadily growing interest over the recent years. For good reason, since these innovative algorithms and methods, such as machine learning and deep neural networks, in which knowledge is acquired and applied based on data, enable the automation of a wide range of processes and quickly deliver precise results. AI is also getting more and more popular in the space sector. The Institute of Space Technology & Space Applications (ISTA) at the Universität der Bundeswehr in Munich is conducting research around AI for space operations, science, and technology. An overview of activities and current developments towards fault management, autonomous collision avoidance, autonomous landing, as well as radio science at ISTA will be presented.
Kinetic Energy Transfer of Near-Earth Objects for Interplanetary Manned Missi...Winston Sanks
This report outlines the rationale, procedures, technical feasibility, risk assessment, and cost-benefit
analysis of utilizing a Near-Earth Object, 101955 Bennu (provisional designation 1999 RQ36 - the target of
the OSIRIS-REx mission), as a source of energy to minimize the propulsion requirements of an
interplanetary spacecraft. The planet Mars is the target body in this study and the outbound Trans-Mars
injection in the years between 2175 and 2199 will be analyzed (within this timeframe Bennu’s orbit is
predicted to approach Earth within two Earth radii on at least 80 occasions). The Mars orbit insertion burn,
Trans-Earth injection burn, and Earth orbit insertion burn are assumed to be achieved with propulsive
maneuvers outlined in standard manned interplanetary mission architectures. To accomplish this mission,
two methods of transferring kinetic energy are examined: direct capture and release of the asteroid by a
spacecraft using a Kevlar net and an inertial reel, and indirect capture by establishing a station on the
asteroid to manufacture compressed material from the carbonaceous regolith in order to fire a mass stream
to be captured by the spacecraft. This mission architecture analysis takes into account the associated safety
risks of perturbations within Bennu’s orbit (which could result in inaccurate rendezvous location
predictions), the implications of altering the orbit of 101955 Bennu after transferring a portion of its energy
(since there is a possibility of collision with Earth in the late 22nd century if the asteroid is slowed too
significantly), g-limit restrictions of the spacecraft and its occupants during an acceleration by the asteroid,
and the possibility of a collision between Bennu and the spacecraft. In addition, the cost-benefit
considerations of this mission architecture are weighed. This examination concludes that a direct capture Net
and Reel system aboard the spacecraft is not a viable capture method due to an insufficient maximum ΔV
available through a best-case perfectly elastic collision (capture) with the asteroid, as well as a prohibitive
weight penalty aboard the spacecraft due to the Net and Reel system. However, this report finds that the
method of establishing a station on Bennu with the capability to separate mass from the asteroid and fire it at
a spacecraft is a plausible (if costly) means of transferring a significant ΔV. A KETNEO-FIMM Asteroid
Station mission architecture could also be used in subsequent interplanetary missions providing cost-sharing
over many decades for future interplanetary missions.
This content presents for basic of Synthetic Aperture Radar (SAR) including its geometry, how the image is created, essential parameters, interpretation, SAR sensor specification, and advantages and disadvantages.
Artificial intelligence (AI) is experiencing steadily growing interest over the recent years. For good reason, since these innovative algorithms and methods, such as machine learning and deep neural networks, in which knowledge is acquired and applied based on data, enable the automation of a wide range of processes and quickly deliver precise results. AI is also getting more and more popular in the space sector. The Institute of Space Technology & Space Applications (ISTA) at the Universität der Bundeswehr in Munich is conducting research around AI for space operations, science, and technology. An overview of activities and current developments towards fault management, autonomous collision avoidance, autonomous landing, as well as radio science at ISTA will be presented.
Kinetic Energy Transfer of Near-Earth Objects for Interplanetary Manned Missi...Winston Sanks
This report outlines the rationale, procedures, technical feasibility, risk assessment, and cost-benefit
analysis of utilizing a Near-Earth Object, 101955 Bennu (provisional designation 1999 RQ36 - the target of
the OSIRIS-REx mission), as a source of energy to minimize the propulsion requirements of an
interplanetary spacecraft. The planet Mars is the target body in this study and the outbound Trans-Mars
injection in the years between 2175 and 2199 will be analyzed (within this timeframe Bennu’s orbit is
predicted to approach Earth within two Earth radii on at least 80 occasions). The Mars orbit insertion burn,
Trans-Earth injection burn, and Earth orbit insertion burn are assumed to be achieved with propulsive
maneuvers outlined in standard manned interplanetary mission architectures. To accomplish this mission,
two methods of transferring kinetic energy are examined: direct capture and release of the asteroid by a
spacecraft using a Kevlar net and an inertial reel, and indirect capture by establishing a station on the
asteroid to manufacture compressed material from the carbonaceous regolith in order to fire a mass stream
to be captured by the spacecraft. This mission architecture analysis takes into account the associated safety
risks of perturbations within Bennu’s orbit (which could result in inaccurate rendezvous location
predictions), the implications of altering the orbit of 101955 Bennu after transferring a portion of its energy
(since there is a possibility of collision with Earth in the late 22nd century if the asteroid is slowed too
significantly), g-limit restrictions of the spacecraft and its occupants during an acceleration by the asteroid,
and the possibility of a collision between Bennu and the spacecraft. In addition, the cost-benefit
considerations of this mission architecture are weighed. This examination concludes that a direct capture Net
and Reel system aboard the spacecraft is not a viable capture method due to an insufficient maximum ΔV
available through a best-case perfectly elastic collision (capture) with the asteroid, as well as a prohibitive
weight penalty aboard the spacecraft due to the Net and Reel system. However, this report finds that the
method of establishing a station on Bennu with the capability to separate mass from the asteroid and fire it at
a spacecraft is a plausible (if costly) means of transferring a significant ΔV. A KETNEO-FIMM Asteroid
Station mission architecture could also be used in subsequent interplanetary missions providing cost-sharing
over many decades for future interplanetary missions.
This content presents for basic of Synthetic Aperture Radar (SAR) including its geometry, how the image is created, essential parameters, interpretation, SAR sensor specification, and advantages and disadvantages.
Noise Removal in SAR Images using Orthonormal Ridgelet TransformIJERA Editor
Development in the field of image processing for reducing speckle noise from digital images/satellite images is a challenging task for image processing applications. Previously many algorithms were proposed to de-speckle the noise in digital images. Here in this article we are presenting experimental results on de-speckling of Synthetic Aperture RADAR (SAR) images. SAR images have wide applications in remote sensing and mapping the surfaces of all planets. SAR can also be implemented as "inverse SAR" by observing a moving target over a substantial time with a stationary antenna. Hence denoising of SAR images is an essential task for viewing the information. Here we introduce a transformation technique called ―Ridgelet‖, which is an extension level of wavelet. Ridgelet analysis can be done in the similar way how wavelet analysis was done in the Radon domain as it translates singularities along lines into point singularities under different frequencies. Simulation results were show cased for proving that proposed work is more reliable than compared to other de-speckling processes, and the quality of de-speckled image is measured in terms of Peak Signal to Noise Ratio and Mean Square Error
Noise Removal in SAR Images using Orthonormal Ridgelet TransformIJERA Editor
Development in the field of image processing for reducing speckle noise from digital images/satellite images is a challenging task for image processing applications. Previously many algorithms were proposed to de-speckle the noise in digital images. Here in this article we are presenting experimental results on de-speckling of Synthetic Aperture RADAR (SAR) images. SAR images have wide applications in remote sensing and mapping the surfaces of all planets. SAR can also be implemented as "inverse SAR" by observing a moving target over a substantial time with a stationary antenna. Hence denoising of SAR images is an essential task for viewing the information. Here we introduce a transformation technique called ―Ridgelet‖, which is an extension level of wavelet. Ridgelet analysis can be done in the similar way how wavelet analysis was done in the Radon domain as it translates singularities along lines into point singularities under different frequencies. Simulation results were show cased for proving that proposed work is more reliable than compared to other de-speckling processes, and the quality of de-speckled image is measured in terms of Peak Signal to Noise Ratio and Mean Square Error.
Application of Remote Sensing in Civil EngineeringIEI GSC
Presentation cum talk delivered by Dr Anjana Vyas, Dean CEPT University, Ahmedabad during 31st National Convention of Civil Engineering organized by The Institution of Engineers (India) Gujarat State Center, Ahmedabad
A coupled Electromagnetic-Mechanical analysis of next generation Radio Telesc...Altair
This work considers the design of large and complex receivers used in the field of radio astronomy, e.g. for the Square Kilometer Array (SKA) project. The purpose of this work is to consider a coupled simulation where the electromagnetic analysis, performed with the computational electromagnetic software package FEKO, is enhanced by the structural analysis offered by HyperWorks products such as HyperMesh and Optistruct. External influences such as gravity, wind-loading and thermal properties will be taken into account. This will enhance the electromagnetic simulation results, thereby aiding designers to mitigate these environmental effects.
Speakers
Dr. Danie Ludick, Postdoctoral researcher, Stellenbosch University
SAR is a type of radar which works with antenna and receiver using radio waves which can create two dimension or three dimension of the objects . A synthetic-aperture radar is an imaging radar mounted on a moving platform. SAR gives high resolution data and works 24*7.
International Journal of Engineering Research and Applications (IJERA) is an open access online peer reviewed international journal that publishes research and review articles in the fields of Computer Science, Neural Networks, Electrical Engineering, Software Engineering, Information Technology, Mechanical Engineering, Chemical Engineering, Plastic Engineering, Food Technology, Textile Engineering, Nano Technology & science, Power Electronics, Electronics & Communication Engineering, Computational mathematics, Image processing, Civil Engineering, Structural Engineering, Environmental Engineering, VLSI Testing & Low Power VLSI Design etc.
The globalization and its impacts, political economy followed by how the globalization and political economy can affect the development of metropolitan cities of the world and the most fascinating part of the presentation which is based upon the case study of Tokyo, Japan that completely seems, the influence globalization and political economy in the city and as last concluding with the future of the urbanization.
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2. Demographic Transition Theory.
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4. Understanding India’s Demographic Transition.
5. Demographic Dividend.
6. Opportunities for India caused by the Demographic Dividend.
7. Challenges faced by India.
8. State-wise trends in the Demographic Transition.
9. Results in terms of Statistics.
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Development in the field of image processing for reducing speckle noise from digital images/satellite images is a challenging task for image processing applications. Previously many algorithms were proposed to de-speckle the noise in digital images. Here in this article we are presenting experimental results on de-speckling of Synthetic Aperture RADAR (SAR) images. SAR images have wide applications in remote sensing and mapping the surfaces of all planets. SAR can also be implemented as "inverse SAR" by observing a moving target over a substantial time with a stationary antenna. Hence denoising of SAR images is an essential task for viewing the information. Here we introduce a transformation technique called ―Ridgelet‖, which is an extension level of wavelet. Ridgelet analysis can be done in the similar way how wavelet analysis was done in the Radon domain as it translates singularities along lines into point singularities under different frequencies. Simulation results were show cased for proving that proposed work is more reliable than compared to other de-speckling processes, and the quality of de-speckled image is measured in terms of Peak Signal to Noise Ratio and Mean Square Error.
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This work considers the design of large and complex receivers used in the field of radio astronomy, e.g. for the Square Kilometer Array (SKA) project. The purpose of this work is to consider a coupled simulation where the electromagnetic analysis, performed with the computational electromagnetic software package FEKO, is enhanced by the structural analysis offered by HyperWorks products such as HyperMesh and Optistruct. External influences such as gravity, wind-loading and thermal properties will be taken into account. This will enhance the electromagnetic simulation results, thereby aiding designers to mitigate these environmental effects.
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Population Pyramid.
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Stats / Graphs of India – with referencing to Population and Demography.
India’s population projection.
Bibliography.
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http://sandymillin.wordpress.com/iateflwebinar2024
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1. ARGHYADEEP SAHA
BSc (Hons.) in Geography (2019 - 2022)
ADAMAS UNIVERSITY, KOLKATA, INDIA
INTERN at GRAPHY BY UNACADEMY, INDIA
Fundamentals of
Remote Sensing
Visit - https://arghyadeep.graphy.com/ 1
Webinar will start within 2 minutes.
Take your seats.
Animation Courtesy - NASA
3. Visit - https://arghyadeep.graphy.com/ 3
BASIC TERMINOLOGY
Image - A visual delineation of entity.
Analog Image
• Produced over Drawing Sheets.
• Produced by Pictographic Detectors.
• Might delineate as Gray Sheds.
Digital Image
• Bring out by Electro-Perceptible.
• Composed of Array of Square
Boxes.
4. Visit - https://arghyadeep.graphy.com/ 4
DIGITAL IMAGE
Source – Google Earth
• Composed of pixels.
• Each pixel has an associated values.
• Pixels / Square boxes with high brightness is of
higher number and vice versa.
• Gray level which is a record of variation in
radiant energy in discreate form.
Source – DN values
obtained from C
5. Visit - https://arghyadeep.graphy.com/ 5
REMOTE SENSING
Remote sensing is the collection of data about the object and environment without being in direct physical contact with the
object.
Light hits the retina → Photoreceptors turn the Light into Electrical Signals → These electrical signals
travel from the retina through the optic nerve to the brain → Then the brain turns the signals into
the images we see.
This phenomenon will work under the limitation to visible region of Electro Magnetic Spectrum.
0.4 – 0.7 μm
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EMR
E LE CT RO MAGNE T I C RADI AT I ON
• Form of energy, transported through space in the form of periodic disturbances
of electric and magnetic fields.
• Travel with the speed of light ; c = 299792458 m/s ≈ 3x108 m/sec.
• Speed of light = frequency x wavelength.
→
E = Electric Field
→
B = Magnetic Field
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EMR
E LE CT RO MAGNE T I C RADI AT I ON
Relationship between Wavelength (λ) and Frequency (v) for
Electromagnetic Waves. (JAMES CLERK MAXWELL)
v=c/λ where, c is the speed of light.
Where, h = 6.626 x 10-34 (Planck’s Constant)
Relationship between Energy (E) and Frequency (v) for
Electromagnetic Waves.
E =hv
Considering,
v = c/λ
E = hc/v
Hence, shorter wavelengths have high energy and vice versa.
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EMR
ELECTRO MAGNETIC RADIATION
Stephen Boltzmann Law:
This law states that the energy emitted by a blackbody per second is the product of the emissivity of that body, the
Stefan-Boltzmann constant, the surface area of the body and the fourth power of the absolute temperature of that body.
Total Emitted Radiation – σT4
Where, σ = 5.6697 x 10-8 W.m-2 .K-4 (Stephen-Boltzmann constant)
Important –
• ‘0’ → Perfect Reflecting Body.
• ‘1’ → Perfect Blackbody.
• ‘0’ / ‘1’ → Natural Body.
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WIEN’S DISPLACEMENT LAW
λmaxT = 2897.9 μmK
T = absolute temperature
The relationship between peak wavelength of emittance
and the temperature of the material.
12. Visit - https://arghyadeep.graphy.com/ 12
Reflection
Visible
VNIR
SWIR
Thermal Infrared
Microwaves
Emission
Back Scattering
EWR
ELECTROMAGNETIC
WAV E LE NG T H RA NG E
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ELEMENTS INVOLVED
IN REMOTE SENSING
Irradiance
Scattered
Radiation
R e f l e c t i o n P r o c e s s
Thermal Emission
ATM Emission
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TYPES OF ORBITS
Credit - The European Organization for the
Exploitation of Meteorological Satellites.
Polar Orbiting Satellites –
• Inclination between 80° - 100°.
• The satellite passes North-South or vv.
• 14 Orbits/day.
Used –
• Earth’s Explorations.
17. Visit - https://arghyadeep.graphy.com/ 17
TYPES OF ORBITS
Credit - Wikipedia.
Geostationary / Geosynchronous Satellites –
• Circular orbit and orbital period is synchronized with rotation period of earth.
• Repeating ground track – fixed paths
Sun-synchronous –
• Satellite passes over the same part of the Earth at roughly the same local
time each day .
• Two fixed times: day and night.
Used –
• Weather Monitoring.
• Tele – Communications.
• Broadcasting.
• Defense Purpose.
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TYPES OF ORBITS
Low inclination orbits –
• Orbit altitude is 160 km.
• Orbital period is about 87 - 88 minutes.
Used –
• Acquiring Images.
• High Spatial Resolution.
Credit – NASA Earth Observatory.
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PLATFORMS
S p a c e B o r n e A i r B o r n e G r o u n d B a s e d
S p a c e S h u t t l e
7
0
0
–
9
0
0
k
m
S a t e l l i t e
1
8
5
–
5
7
5
k
m
A i r c r a f t w i t h S A R
D r o n e w i t h S A R
1
0
–
1
2
k
m
1
0
0
–
1
5
0
m
S p e c t r o r a d i o m e t e r
20. Visit - https://arghyadeep.graphy.com/ 20
IMAGE REFERENCING SYSTEM
• Is a referencing system for locating satellite image
scenes.
• Path is the descending orbit of the satellite.
• Row refers to the latitudinal center line of a frame of
imagery.
• The Path number is always given first, followed by the
Row number.
Example –
The notation 129-051, for example, relates to
Path number 129 and Row number 051.
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APPLICATIONS OF REMOTE
SENSING IMAGES
Lithological Mapping –
• The lithologically bound epigenetic /syngeneic deposits are formed due to strong preference of host rocks.
Credit – RS Dept. Geological Survey of India (GSI)
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APPLICATIONS OF REMOTE
SENSING IMAGES
Zone Mapping –
• Hydrothermal alteration is commonly indicated and can be explored through RS.
Credit – RS Dept. Geological Survey of India (GSI)
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APPLICATIONS OF REMOTE
SENSING IMAGES
River Morphology –
NASA recently released these images of the Padma River’s transformation over three decades in Bangladesh. Satellite imagery shows how the river has been
transforming in shape, size, and location from 1988 to 2018.
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APPLICATIONS OF REMOTE
SENSING IMAGES
Land Use Land Cover Map –
Land use and Land Cover map of Maharashtra, India, during 2013-2014
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APPLICATIONS OF REMOTE
SENSING IMAGES
Planetary Exploration –
Image Credit: NASA/Goddard Space Flight Center/DLR/ASU
Published: October 5, 2017
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CAPABILITY OF REMOTE SENSING
• Secular Images
• Large Spatial Blanket
• Access to inaccessible areas
• Sensitive to wavelength region beyond → 0.4 μm to 0.7 μm
• Space Exploration
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CLASSES OF RESOLUTION
Spatial Resolution –
Animation Courtesy – G World
• The earth surface area covered by a pixel of an image is known as spatial resolution.
High Spatial Resolution
Low Spatial Resolution
30. Visit - https://arghyadeep.graphy.com/ 30
CLASSES OF RESOLUTION
Temporal Resolution –
• Frequency at which images are recorded / captured in a specific place on the earth.
• The Landsat series of satellites have a repeat period ranging from 16 – 18 days, whereas in the case of IRS, it is 22 days.
Credit – Dr. Ranganath Ramarao Navalgund, Director & Distinguished Scientist, Space Application Centre, ISRO ( 2005-2012 )
Banda Aceh, Indonesia, Before December 2004 Banda Aceh, Indonesia, After December 2004
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CLASSES OF RESOLUTION
Spectral Resolution –
• Spectral Resolution is the range of wavelength that satellite imaging system can detect.
• It refers to the width and number of spectral bands.
• Describes the specific wavelength intervals in the EMR that a sensor can record.
Spectral Profile
Value
Wavelength
Low Spectral Resolution
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CLASSES OF RESOLUTION
Three types of Spectral Resolution –
PA N C H R O M AT I C M U LT I S P E C T R A L H Y P E R S P E C T R A L
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CLASSES OF RESOLUTION
Radiometric Resolution
• Sensitivity of the sensor to the magnitude of the received electromagnetic energy determines the radiometric resolution.
• Finer the radiometric resolution of a sensor, if it is more sensitive in detecting small differences in reflected or emitted
energy.
1 bit 2 bit 4 bit
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SENSOR TECHNOLOGY
CLA SSE S O F SE NSO RS FO R G E NE RAT I NG
I MAGE S
Whisk Broom Imaging Sensors: Across-Track
Credit – Dr. Ranganath Ramarao Navalgund, Director & Distinguished Scientist, Space Application Centre, ISRO ( 2005-2012 )
37. Visit - https://arghyadeep.graphy.com/ 37
SENSOR TECHNOLOGY
CLA SSE S O F SE NSO RS FO R G E NE RAT I NG
I MAGE S
Push Broom Imaging Sensors: Along-Track
Credit – Dr. Ranganath Ramarao Navalgund, Director & Distinguished Scientist, Space Application Centre, ISRO ( 2005-2012 )
38. Visit - https://arghyadeep.graphy.com/ 38
SENSOR TECHNOLOGY
CLA SSE S O F SE NSO RS FO R G E NE RAT I NG
I MAGE S
Push Broom Imaging Sensors: Along-Track (Frame Capture)
Credit – Dr. Ranganath Ramarao Navalgund, Director & Distinguished Scientist, Space Application Centre, ISRO ( 2005-2012 )
39. THANK YOU !
I F ANY QUE ST I ONS ?
M A I L M E – a rg h ya d e e p . s a h a @ s t u . a d a m a s u n i ve rs i t y. a c . i n ( O f f i c i a l )
rg h d p s a h a @ g m a i l . c o m ( Pe rs o n a l )
Webinar Organized By –
GRAPHY by UN AC ADEMY, I N DI A
Name – Arghyadeep Saha
Ed u cation al Bac kg rou n d – BS c ( Hon s .) in Geog rap hy. ( Pu rsu in g ) .
Ed u cation al In stitu tion – A d amas Un iversity, Kolkata, IN .
Comp lementar y S ubjec ts – Math emati c s ; Econ omic s ; Comp u ter S c ien c e an d
A p p lication s .
Skil ls & endorseme nts – C ( Basic) , C+ + (Advanced) , Remote Sensing and
Geoinformatic s ; Qu antu m GIS ( Profession al) ,S p read sh eets, Doc s, S lid es .
Presently obtain in g skills – MATLA B, R , A RC GIS , P y th on , Goog le Earth E n g in e .
S pecial Appreciations –
Dr. Hrishikesh S amant
( A s s t . P r o f / V i c e P r i n c i p a l , S t . Xa v i e r ' s C o l l a g e , M u m b a i , I n d i a )
Dr. Ranganath Ramarao N avalgund
( F o r m e r ) D i r e c t o r & D i s t i n g u i s h e d S c i e n t i s t , S p a c e A p p l i c a t i o n C e n t r e , I S R O
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