Training Course Remote Sensing – Basic Theory & Image ...drm.cenn.org/Trainings/Remote...

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9/12/2011 1 Training Course Remote Sensing – Basic Theory & Image Processing Methods 19 – 23 September 2011 Remote Sensing Platforms Remote Sensing Platforms Remote Sensing Platforms Remote Sensing Platforms Michiel Damen Michiel Damen (September 2011) (September 2011) [email protected] [email protected] [email protected] [email protected]

Transcript of Training Course Remote Sensing – Basic Theory & Image ...drm.cenn.org/Trainings/Remote...

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Training CourseRemote Sensing – Basic Theory & Image Processing Methods19 – 23 September 2011

Remote Sensing PlatformsRemote Sensing PlatformsRemote Sensing PlatformsRemote Sensing PlatformsMichiel Damen Michiel Damen (September 2011)(September 2011)

[email protected]@[email protected]@itc.nl

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

OverviewOverview

Platforms & missions aerial surveysaerial surveys satellite

Cameras Scanners Scanners Stereoscopy Questions

Michiel Damen, ITC

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

RS PlatformsRS Platforms

A RS platform is a vehicle, such as a satellite or aircraft that carries one or more RS sensorscarries one or more RS sensorsAir-borne platforms

(100 m. - 8 km altitude)aircraft, or helicopter, , p ,microlight, balloon, etc.

Space-borne platforms(5000 – 36 000 m altitude)(5000 – 36.000 m. altitude)Large or small platforms, Space Shuttle

Michiel Damen, ITC 3

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Aerial Survey missions

Air-borne remote sensing Speed : 150–750 km/hr selected based on sensor system

Aerial Survey missions

Speed : 150–750 km/hr selected based on sensor system

Altitude : 500 m. up to 8 km. Selection based on image scale.

Sensor position determined by (differential) GPS

O i t ti i fl d b i d diti Orientation influenced by wind conditions

Michiel Damen, ITC 4

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Aerial Survey missions

GPS and IMU for direct sensor orientation

Diff ti l Gl b l P iti i S t (GPS) li d f

Aerial Survey missions

Differential Global Positioning System (GPS) applied for more precise positioning. Second GPS within 30 km from the aircraft

Inertial Measuring Unit (IMU) measures the attitude angles of the sensor Assemblage of gyros and accelerometerssensor. Assemblage of gyros and accelerometers.

A i l A i l Aerial cameraAerial camera

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IMUIMU

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Aerial Survey missionsAerial Survey missions

Position of the aircraft

GPS

Attitude of the aircraft IMU

On board GPS

+

+GPS base

station on the ground

Distance between the aircraft and the ‘ground’

+

Michiel Damen, ITC

Angle under which the distance has been measured

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Aerial Survey missions

Acquisition of overlapping aerial photos

Aerial Survey missions

Michiel Damen, ITC 7

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Satellite missions

Orbital characteristics ( I ):

O bit l ltit d di t (i k ) f th t llit t th

Satellite missions

Orbital altitude : distance (in km) from the satellite to the surface of the Earth.

- Low orbit (<1000 km) : Landsat, SPOT, ASTER

- High orbit (36.000 km) : Geostationary

Orbital inclination angle : angle (in degrees) between the orbital plane and the equatorial plane.

Determines , together with the field-of-view (FOV) of the sensor the latitudes up to which the earth can be observed

Michiel Damen, ITC 8

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Satellite missionsSatellite missions

Orbital characteristics ( II ):

Orbital period : time required to complete one full orbit. Polar satellites: 100 min. at 800 km. altitude

Repeat cycle : time (in days) between two successiveRepeat cycle : time (in days) between two successive identical orbits.

Revisit time : time between two subsequent images of the same area, also dependent on the pointing capability of the sensor (for instance SPOT)

Michiel Damen, ITC 9

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Satellite missions

SPOT : increased revisit times due to side looking

Satellite missions

g

Michiel Damen, ITC 10

Figures: Drury, Image Interpretation in Geology

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Satellite missions

Orbital types

P l bit bit ith i li ti l b t 80

Satellite missions

Polar orbit : orbit with inclination angle between 80 and 100 degrees

Sun-synchronous orbit : near-polar orbit chosen in h th t th t llit h dsuch a way that the satellite passes overhead

at the same time : Landsat, SPOT, IRS, ASTER.

Geostationary orbit : satellite placed above equator t ltit d f 36 000 kat an altitude of approx. 36.000 km.

Michiel Damen, ITC 11

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Satellite missions

Market figures Currently around 20 space-borne optical sensor systems operational

Satellite missions

y p p y p

Three radar based space-borne systems available

Various civil RS satellite launched every year

Aerial survey oldest RS technique Aerial survey oldest RS technique

New types of sensors:

o air-borne laser scanners Formosat -2o air-borne hyper-spectral sensors

Michiel Damen, ITC 12

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Satellite missions

Digital cameras

A di it l i l t ti l t

Satellite missions

A digital camera is an electro-optical remote sensor The CCD array can either be an assembly of linear arrays

or a matrix array. Three channels for Red Green and Blue coloursThree channels for Red, Green and Blue colours Matrix array used for small format frame cameras (a) Linear array used for moving RS sensors (b)

Michiel Damen, ITC 13

aa bb

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Course: Remote Sensing – Basic Theory & Image Processing Methods - 19 - 23 September 2011

Satellite missions - Linear array sensorSatellite missions Linear array sensor

First satellite with line camera :SPOT 1 (1986)Linear detector array

OpticsSatellite

SPOT 1 (1986)

orbitp

Field of View (FOV)

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Satellite missions - Linear array sensor

The Aster has two sensors in the VNIR: one “nadir” looking and another one “backward” looking

Satellite missions Linear array sensor

g

Stereo images can be produced in ASTER using both nadir and backward looking images

ASTER

Nadir

ASTERSensor

Michiel Damen, ITC 15

Backward

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RS Scanners

Electro-optical RS with a mechanical component. IFOV: Instantaneous FOV (2.5 mrad or less).

RS Scanners

( ) Use in VIS, NIR, TIR One detector per band and a prism splits the light into

wavelengths.

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RS Scanners

Scanner

RS Scanners

Scanner

FOV

IFOV

Swath width

Swath widths- Landsat : 185 km- Aster: 60 km

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RS Scanners - Problems

Problem: different CCDs in the array may be degrade or be out of order

RS Scanners Problems

be out of order

Regular calibration needed

Landsat 7

Michiel Damen, ITC 21

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Stereoscopy – anaglyph vision

Science of producing three-dimensional (3D) visual models

Stereoscopy anaglyph vision

Basic requirements: images of the same object from two different positions

Can be viewed at the computer screenCan be viewed at the computer screen Anaglyph : red & blue (or green)

Michiel Damen, ITC 22

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Stereoscopy (2) - screenscope

I ILWIS ft 3D i li ti ibl b bi i• In ILWIS software 3D visualization possible by combininga. overlapping aerial photographsb. drape of image over DEM

Examples:p- Landsat & SRTM

- Aster VNIR & DEM- “Google” image &

LidLidar

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Stereoscopy – Remote sensorsStereoscopy Remote sensors

Along track

Aerial photos

Across track

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Across track

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Questions

Michiel Damen, ITC 25