Remote Sensing Review Lecture 1 What is remote sensing Remote Sensing: remote sensing is science of acquiring, processing, and interpreting images and related data that are obtained from ground-based, air-or space-borne instruments that record the interaction between matter (target) and electromagnetic radiation. Remote Sensing: using electromagnetic spectrum to image the land, ocean, and atmosphere. Electromagnetic Spectrum Source: http://oea.larc.nasa.gov/PAIS/DIAL.html Ways of Energy Transfer Energy is the ability to do work. In the process of doing work, energy is often transferred from one body to another or from one place to another. The three basic ways in which energy can be transferred include conduction, convection, and radiation. • Most people are familiar with conduction which occurs when one body (molecule or atom) transfers its kinetic energy to another by colliding with it (physical contact). This is how a pan gets heated on a stove. • In convection, the kinetic energy of bodies is transferred from one place to another by physically moving the bodies. A good example is the convectional heating of air in the atmosphere in the early afternoon (less dense air rises). • The transfer of energy by electromagnetic radiation is of primary interest to remote sensing because it is the only form of energy transfer that can take place in a vacuum such as the region between the Sun and the Earth. Jensen, 2000 Wave model of EMR Electromagnetic wave consists of an electrical field (E) which varies in magnitude in a direction perpendicular to the direction in which the radiation is traveling, and a magnetic field (M) oriented at right angles to the electrical field. Both these fields travel at the speed of light (c). Jensen, 2000 Three characteristics of electromagnetic wave Velocity is the speed of light, c=3 x 108 m/s wavelength ( )גis the length of one wave cycle, is measured in metres (m) or some factor of metres such as centimetres (cm) 10-2 m micrometres (µm) 10-6 m nanometres (nm) 10-9 m Frequency (v) refers to the number of cycles of a wave passing a fixed point per unit of time. Frequency is normally measured in hertz (Hz), equivalent to one cycle per second, and various multiples of hertz. unlike c and גchanging as propagated through media of different densities, v remains constant. Hertz (Hz) 1 kilohertz (KHz) 103 megahertz (MHz) 106 gigahertz (GHz) 109 The amplitude of an electromagnetic wave is the height of the wave crest above the undisturbed position Travel time from the Sun to Earth is 8 minutes Particle model of EMR Sir Isaac Newton (1704) was the first person stated that the light had not only wavelike characteristics but also light was a stream of particles, traveling in straight lines. Niels Bohr and Max Planck (20’s) proposed the quantum theory of EMR: Energy content: Q (Joules) = hv (h is the Planck constant 6.626 x 10 –34 J s) = c/v=hc/Q or Q=hc/ The longer the wavelength, the lower its energy content, which is important in remote sensing because it suggests it is more difficult to detect longer wavelength energy Newton’s experiment in 1966 Energy of quanta (photons) Jensen, 2000 EMR details (mm) •Red: 0.620 - 0.7 •Orange: 0.592 - 0.620 •Yellow: 0.578 - 0.592 •Green: 0.500 - 0.578 •Blue: 0.446 - 0.500 Bees and some other insects can see near UV. The Sun is the source of UV, but only > 0.3 mm (near UV) can reach the Earth. •Violet: 0.4 - 0.446 EMR details (2) Source of EMR All objects above absolute zero emit electromagnetic energy, including water, soil, rock, vegetation, and the surface of the Sun. The Sun represents the initial source of most of the electromagnetic energy remote sensing systems (except radar and sonar) Total radiation emitted M (Wm–2) = σT4 (Stefan-Boltzmann Law), where T is in degrees K and σ is the “Stefan-Boltzmann” constant, 5.67×10–8 K–4Wm–2 -- Energy at Sun enormous, 7.3×107 Wm–2, reduced to 459 Wm–2 by Earth-Sun distance Wavelength λmax of peak radiation, in μm = 2897/T (Wien’s Displacement Law) Examples: -- Peak of Sun’s radiation λmax = 2897/6000 = 0.48 μm -- Peak of Earth’s radiation λmax = 2897/300 = 9.7 μm Jensen, 2000 Jensen, 2000 Paths and Interactions If the energy being remotely sensed comes from the Sun, the energy: • is radiated by atomic particles at the source (the Sun), • propagates through the vacuum of space at the speed of light, • interacts with the Earth's atmosphere (3A), • interacts with the Earth's surface (3B), • interacts with the Earth's atmosphere once again (3C), • finally reaches the remote sensor where it interacts with various optical systems, filters, emulsions, or detectors (3D). Various Paths of Satellite Received Radiance Total radiance LS at the sensor Solar irradiance E 0 Lp 90Þ T LT 0 T 2 Diffus e s ky irradiance Remote sens or detector Ed 1 1,3,5 4 v 60 miles or 100km Atmos phere v 0 3 LI 5 Reflectance from neigh boring area, Reflectance from study area, r n r Jensen, 2000 Several concepts Planck’s equation - if a blackbody transforms heat into radiant energy, then the radiation 2hc 2 received at a sensor is given by Planck’s equation. B( , T ) 5 (e hc / kT ) 1) Spectral Emissivity Actual _ Emission / Absorption(Wm 2 mm1 ) e Blackbody _ Emission / Absorption(Wm 2 mm1 ) Spectral reflectivity is the percentage of EMR reflected by the object in a each wavelength or spectral bands Albedo is ratio of the amount of EMR reflected by a surface to the amount of incident radiation on the surface. Fresh Snow has high albedo of 0.80.95, old snow 0.5-0.6, forest 0.1-0.2, Earth system 0.35 EMR EMR EMR 0.6 average shrub 0.5 average grass average soil Reflectance 0.4 0.3 0.2 0.1 0 250 500 750 1000 1250 1500 Wavelength (nm) 1750 2000 2250 2500 Some others Pixel FOV and IFOV Solid angle Radiance Cross track and along track Whiskbroom and Push broom Dwell time Nadir and off-nadir Remote sensing platforms Ground and Aircraft Based Ground repeat or continuous sampling regional or local coverage example: NEXRAD for precipitation Aircraft repeat sampling , any sampling interval regional or local coverage examples: AVIRIS for minerals exploration LIDAR for ozone and aerosols Space Based Sun-synchronous polar orbits Low-inclination, non-Sun-synchronous orbits global coverage, fixed crossing, repeat sampling typical altitude 500-1,500 km example: MODIS, Landsat tropics and mid-latitudes coverage, varying sampling typical altitude 200-2,000 km example: TRMM Geostationary orbits regional coverage, continuous sampling over equator only, altitude 35,000 km example: GOES Types of remote sensing Passive: source of energy is either the Sun, Earth, or atmosphere Sun - wavelengths: 0.4-5 µm Earth or its atmosphere - wavelengths: 3 µm 30 cm Active: source of energy is part of the remote sensor system Radar - wavelengths: mm-m Lidar - wavelengths: UV, Visible, and near infrared Measurement scales constrained by physics and technology Spatial resolution (IFOV/GSD) and coverage (FOV) Spectral resolution (D ) and coverage (min to max) Narrow bands need bigger aperture, more detectors, longer integration time Radiometric resolution (S/N, NEDr, NEDT ) and coverage (dynamic range) Optical diffraction sets minimum aperture size Aperture size, detector size, number of detectors, and integration time Temporal resolution (site revisit) and coverage (global repeat) Pointing agility, period for full coverage Basics of Bit Computer store everything in 0 or 1 Bit no. 7 6 5 4 3 2 1 0 0 0 0 0 0 0 0 0 0 256 1 1 1 1 1 1 1 1 8 bits as an example bits Max. num (2bits) 1 2 3 6 8 11 12 2 4 8 64 256 2048 4096 The size of a cell we call image resolution, depending on… Such as 1 m, 30 m, 1 km, or 4 km Digital Image Data Formats Each band of image is stored as a matrix (array) format; To efficiently handle the multi-bands (and hyperspectral) imagery in an image processing software, BSQ (band sequential), BIL (band interleaved by line), BIP (band interleaved by pixel) are common image data format (see an example in p103 of the text book) . Procedures of image processing Preprocessing Radiometric correction is concerned with improving the accuracy of surface spectral reflectance, emittance, or back-scattered measurements obtained using a remote sensing system. Atmospheric and topographic corrections Geometric correction is concerned with placing the above measurements or derivative products in their proper locations. Information enhancement Point operations change the value of each individual pixel independent of all other pixels Local operations change the value of individual pixels in the context of the values of neighboring pixels. They are image reduction, image magnification, transect extraction, contrast adjustments (linear and non-linear), band ratioing, spatial filtering, fourier transformations, principle components analysis, and texture transformations Information extraction Post-classification Information output Image or enhanced image itself, thematic map, vector map, spatial database, summary statistics and graphs Remote Sensing Applications Land: rocks, minerals, faults, land use and land cover, vegetation, DEM, snow and ice, urban growth, environmental studies, … Ocean: ocean color, sea surface temperature, ocean winds, … Atmosphere: temperature, precipitation, clouds, ozone, aerosols, … Applications driving remote sensing 107 8 5 Jensen, 2000 3 2 I 106 8 5 30 II 10 8 7 6 5 4 3 III 2 1 0.8 0.7 0.6 0.5 IV 0.4 3 2 105 8 5 Temporal Resolution in minutes Various application demands as driving forces for the resolution improvemen ts of remote sensing 20 Nominal Spatial Resolution (ground resolved distance, meters) 1m 0.3 0.5 100 80 70 60 50 40 3 2 104 8 5 3 15 y 10 y 5y 4y 3y 2y 1y 10 8 5 0.2 L2 S1 100 m Jensen, 2000 LI L3 E1 B1 D E1, E2 T2 U2 U3 T1, U1 L4 C1 SPOT HR V 1,2,3,4 Pan 10 x10 MSS 20 x20 SPOT 5 HR G (2001; not shown) Pan 2.5 x 2.5; 5 x 5 MSS 10 x 10; SWIR 20 x20 180 d C2 55 d 44 d 30 d 26 d 22 d 16 d JERS-1 MSS 18 x 24 L-band 18 x 18 ERS-1,2 C-band 30 x 30 SPIN -2 KVR-1000 2 x 2 TK-350 10 x 10 9d 10,000 min 5d 4d 3d 2d 1d 1,000 min 12 hr IRS-1 AB LISS-1 72.5 x 72.5 LISS-2 36.25 x 36.25 IRS-1C D Pan 5.8 x 5.8 LISS-3 23.5 x 23.5; MIR 70 x 70 Wi FS 188 x 188 LAND SAT 4,5 MSS 79 x 79 TM 30 x 30 LAND SAT 7 ETM + (1999) Pan 15 x15; M SS 30 x 30 TIR 60 x 60 Quickbird (2000) 0.82 x 0.82 3.28 x 3.28 ASTER (1999) EOS AM -1 VNIR 15 x 15 m SWIR 30 x 30 m TIR 90 x 90 m D E3 D E4 D E5 D E2 R AD ARSAT C-band 11-9, 9 25 x28 48-30 x 28 32-25 x 28 50 x50 22-19 x 28 63-28 x 28 100 x100 M5 EOSAT/Space Imaging IKONOS (1999) Pan 1 x 1 MSS 4 x 4 IRS-P5 ( 1999) Pan 2.5 x 2.5 1 hr I II III IV Land Cover Class Level ORB IMAGE OrbView 2 SeaW iFS 1.13 x 1.13 km AVHR R LAC 1.1 x 1.1 km GAC 4 x4 km METEOSAT VISIR 2.5 x2.5 km TIR 5 x 5 km T4 GOES VIS 1 X 1 km TIR 8 x 8 km Aerial Photography < 0.25 x 0.25 m ( 0.82 x0.82 ft.) 1 x1 m (3.28 x 3.28 ft.) min M1 M2 N WS WSR -88D D oppler R adar 1 x1 km 4 x4 km T3 3 2 0.1 SPOT 4 Vegetation 1 x1 km MODIS (1999) EOS AM -1 Land 0.25 x0.25 km Land 0.50 x0.50 km Ocean 1 x 1 km Atmo 1 x 1 km TIR 1 x 1 km ORB IMAGE OrbView 3 (1999) Pan 1 x 1 MSS 4 x 4 OrbView 4 (2000) Pan 1 x 1 MSS 4 x 4 H yperspectral 8 x 8 m 100 min 3 2 0.3 20 30 S2 3 2 102 8 5 10 S3 D1 D2 2 103 8 5 5 1m 2 3 5 10 15 20 30 0.2 0.3 0.5 .8 1.0 2 3 5 10 2 3 1 km 1000 m 100 m 5 102 2 3 Nominal Spatial Resolution in meters 5 103 M3 M4 5 km 10 km 2 34 5 8 104 From Terra, Aqua to NPP to JPSS Terra (1999) Aqua (2002) NPP (2011, Oct) Coriolis (2003) WindSat METOP (2006) IASI/AMSU/MHS & AVHRR AIRS, AMSU & MODIS CrIS/ATMS VIIRS OMPS JPSS/ (2016, 2019) CrIS/ATMS, VIIRS, CMIS, OMPS & ERBS Use of Advanced Sounder Data for Improved Weather Forecasting & Numerical Weather Prediction NOAA Real-Time Data Delivery Timeline Ground Station Scenario NWS/NCEP GSFC/DAO ECMWF C3S IDPS NOAA Real-time User UKMO FNMOC Meteo-France BMRC-Australia Joint Center for Satellite Data Assimilation Met Serv Canada NWP Forecasts NPP Goals The NPP mission has two major goals: To provide a continuation of the EOS record of climate- quality observations after EOS Terra, Aqua, and Aura (i.e., it will extend key Earth system data records and/or climate data records of equal or better quality and uncertainty in comparison to those of the Terra, Aqua, and Aura sensors), and To provide risk reduction for JPSS instruments, algorithms, ground data processing, archive, and distribution prior to the launch of the first JPSS spacecraft (but note that there are now plans to use NPP data operationally) 29 NPP sensors NPP Satellite Scheduled for Launch Nadir facing antennas – T&C – HRD – SMD Launched: October 28, 2011 VIIRS CrIS ATMS OMPS http://jointmission.gsfc.nasa.gov/ 31 Data Products Level 1 products VIIRS, CrIS, ATMS and OMPS Sensor Data Records (SDRs) are full resolution sensor data that are time referenced, Earth located, and calibrated by applying the ancillary information, including radiometric and geometric calibration coefficients and georeferencing parameters such as platform ephemeris. These data are processed to sensor units (e.g., radiances). Calibration, ephemeris, and other ancillary data necessary to convert the sensor data back to sensor raw data (counts) are included. Level 2 (EDR/CDRs) products EDR emphasis will be on generating products with a more rapid data delivery that necessarily involves high-speed availability of ancillary data and high-performance execution of the sensor contractors' state-of-the-art science algorithms for civilian and military applications. CDR, the requirement of timeliness can be relaxed, thereby allowing for the implementation of complex algorithms using diverse ancillary data. As understanding of sensor calibration issues and radiative transfer from the Earth and Atmosphere improves, algorithms can be improved, and products can be generated via reprocessing EDR: environmental data records Major image processing software ENVI/IDL: http://www.rsinc.com/ ERDAS Imagine: http://www.gis.leicageosystems.com/Products/Imagine/ PCI Geomatics: http://www.pci.on.ca/ ER Mapper: http://www.ermapper.com/ INTEGRAPH: http://imgs.intergraph.com/gimage/ IDRIS: Ecognition: http://www.definiensimaging.com/ecognition/pro/40.htm See5 and decision tree