lidarprimer - collins
TRANSCRIPT
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A LiDAR Primer
Richard L CollinsGeophysical Institute and Department
of Atmospheric SciencesUniversity of Alaska Fairbanks
February 15, 2011
Kenai GIS User Group
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Lidar studies in 1930’s using
search lights. Use of lasers
since the 1960’s.
Used in a wide variety of both
civilian and military
applications;• Biohazards
• Fisheries
• Forestry
•
Fire
•
Glaciology
•
Mapping
• Meteorology
• Pollution
• Space Surveillance
LiDAR – Light Detection And Ranging
Lidar Firsts – From “Airborne andSpaceborne Lidar” M. P. McCormick,2005.
CALIPSO 2007
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LITE – LiDAR In-space Technology Experiment
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Contemporary LiDAR System Concept
650 m widescan swath
30°scanangle
1200 mflight
altitude
1.5 m
1.5 m
IMU
GPSgroundstation
DifferentialGPS
navigation
GPS satellites
Optech ALTM
Airborne LiDAR
± 15 cm
vertical
accuracy
30 cm widelaser
footprint
Topographic Laser Ranging and Scanning:Principles and Processing Shan, J, and C.K. Toth, CRC Press, 2009.
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Optech’s Gemini Airborne Laser Terrain Mapper System
Range 150-4000 mWavelength 1064 nmElevation accuracy 5-35 cm
PRF 33 - 167 kHzPosition GPS and GLONASS
Scan Width 0-50°San Rate 0 - 70 Hz
Range Capture < 4 returnsDivergence 0.25/0.8 mrad
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Hand-held Laser Scanners - Helimap
Heigel laser scanning engine withHasselblad digital frame camera.Rigid carbon fiber frame withhandles.System IMU in box below thecamera.
Helimap system being operated from side ofAlouette III helicopter. System allowsaccurate and high resolution mapping ofsteep and narrow terrain.
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LiDAR Comes of Age
Lidar systems were developed as research systems since the 1960’s.
Terrestrial lidar systems come of age in the 1990’s as several enabling
technologies mature;1.
Fully solid-state lasers where solid-state lasers (e.g., Nd:YAG,
Nd:YLF) pumped by laser diodes
2.
High-speed electronics and computers
3.
A mature Global Positioning System
The following elements are found in contemporary lidar systems
1.
Laser Ranging Unit
2.
Optical Scanning Mechanism
3.
Electronic and Computer Unit4. Position and Orientation Unit
5. Software6.
Imaging System
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Basic LiDAR System
Laser(s)
Telescope
Beam Expander
Photodiode
Optics -Collimation,
FOV and
BandwidthPhotodiode
BS
Lens
Electronics -
Counting/
Timing and
Threshold
Computer
Basic system composed of;• Laser-based transmitter• Telescope-based receiver• High-speed electronics• Optics•
Computer
Lasers providehigh-intensitysmall-footprintnarrow-bandfrequency-stable
beams for probing the environment.
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Echo Detection and Ranging
Knowing the speed oflight, the range fromthe LiDAR to a targetis determined by theround trip time.
The echo timing isdefined by the
leading edge of thelaser pulse and theecho pulse.
Timing is everything,!R = (!t"v + t"!v)/2
as !v/v is very small.
The thresholddetection can dependon signal amplitude.
Time
R a n g e
R1
R2
t
1
t
2
R = v x t
v x t1 = 2 x R
1v x t
2= 2 x R
2
Time
R e c e i v e d
S i g n a
l
t1
T r a n s m i t t e d
S i g n a l
t0
Threshold
Threshold
!t = t1 - t0
T p
T p
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d1 d2
= d1 + R x !R
Laser beams diverge with distance. Anyfinite beam inherently expands as it
propagates.
The Field-Of-View (FOV) of the receivermust match (or exceed) the divergence ofthe transmitter.
• The FOV determines the amount of
background signal.• The FOV places mechanical stability
requirements on the lidar system.
Beam Divergence and Reflection
Specular Lambertian Diffuse Complex
Surfaces found in nature are rarely a smoothtransition between two homogenous media.
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Energy Link Budget - 1
Ground
dR
AircraftET
Eig Erg
ER
Rg
T T
!
Consider a single laserpulse transmitted froman aircraft.
Follow the round trip.
1. ET
2. Eig = ET " T
3. Erg = Eig " #
4. ER = Erg " T " P
where,
P = " # $ # (dR /2)
2
2# $ # Rg2
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Energy Link Budget-2
The analysis yields a form of the Lidar Equation
ER = " # $ # (dR /2)2
2# $ # Rg2
#T 2%
&
' '
(
)
* *
#ET
Consider an airborne lidar, Rg = 1000 m (3281 ft, 0.6214 mile)
dR = 11.3 cm (4.44 in)
# = 0.5
T = 0.8
$ ER = 5.1 x 10-10 " ET
Consider a satellite lidar (CALIPSO)
Rg = 705 kmdR = 1 m
# = 0.5
T = 0.8
$ ER = 1.6 x 10-13 " ET
ET = 110 mJPRF = 20HzT p = 10 ns% = 532 nm &
1064 nm& = 130 µrad
ET = 20 µJPRF = 100 KHz
T p = 10 ns% = 1064 nm,
1550 nm& = 0.2 – 1 mrad
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Energy Link Budget-3
80-90%
~50%
F r e s h S n o w
G r a s s , L i g h t s o i l
~10% ~15%~25%
L a k e
C o n c r e t e
A s p h a l t
Reflectivities
at 900 nm
~60%
~30%
D e c i d u o u s T r e e s
C o n i f e r o u s T r e e s
L i m e s t o n e , C l a y
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Profiling
0
Rg
R
a n g e
Aircraft
Ground
H o r i z o n t a l D i s t a n c e
0
xf
2xf
3x
fdg
0
va x T PRF
va x 2 xT PRF
v
a
x 3 xT
PRF
T i
m e
dg
Cessna 337 at 1000 m
and 67 m/s (130 knots).
Profiling (not scanning)
PRF < 150 kHz.
Divergence
& = 0.2 mrad
Footprintdg = 0.2 m
xf > 0.5 mm
Given divergence non-overlap occurs at
xf > dg
PRF = 335 Hz
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Scanning
The scanner extends the scope
of the profiling system to yieldswaths in the transversedirection. A variety of scanningmethods have been implementedusing oscillating and rotatingmirrors.
A Palmer scanner uses a nutatingmotion to yield a scan that yields an elliptical scan. Most ofthe measurement points arescanned twice, once in theforward and once in thebackward view. This redundancycan be used to calibrate thescanner and the position andorientation system.
Topographic Laser Ranging and Scanning:
Principles and Processing Shan, J, and C.
K. Toth, CRC Press, 2009.
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Range Resolution and Range Discrimination-1
The finite rise time of thelaser pulse, tR, determines theprecision with which thethreshold detector operates.
Ideally tR should be as smallas ossible.
The finite width of thelaser pulse, T P,determines theprecision with which
the LiDAR candistinguish between
closely spaced objects.
Ideally T P should be assmall as possible.
Time
R e c e i v e d
S
i g n a l
t1
Threshold
t2
RangeR2R1
t2 - t1 = < T pR2 - R12 x v
!R > 2 x v x T p
0
0
Time
R e c e i v
e d
S i g n a
l
Threshold
0
tR
T P
The need to minimize tR and T P pushes designers to employ high-
speed (i.e., large bandwidth) analog circuits.
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Range Resolution and Range Discrimination–2
Threshold1
Time
!t1
Threshold2
!t2
R e c e i v e d
S i g n a l
Time
R e c e i v e
d
S i g n a l
0 tS
t
R
The slope of the leading
edge may vary due to• signal noise,• pulse amplitude
variations• pulse spreading due to
elevation variations in
the footprint.
Full-waveform samplingcaptures the shape of theentire signal, not just theleading edge.
The approach supports more
information at GREAT costin both (analog and digital)circuitry and data handling.
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Multiple Returns-1
Topographic Laser Ranging and Scanning:
Principles and Processing Shan, J, and C.
K. Toth, CRC Press, 2009.
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Multiple Returns-2
The lidar echo can contain much more information than is revealed by the multiple
returns detected using a single threshold level.
Full-waveform sampling captures the complete echo but increases the hardware
data handling costs of the system.
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Terrain Mapping-1
The first returns yield the Digital Surface Model (DSM). In vegetated areas the DSM isthe Canopy Top.
The Digital terrain Map (DTM, or bare Earth Surface) is inferred from a spatial filteringthat identifies the lowest returns that define a continuous surface.
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Terrain Mapping-2 Commercial survey in Puget Sound. Lidarfootprint sub-meter diameter, with two
foot rints er s uare meter, and four returns
Topographic Laser Ranging and Scanning:
Principles and Processing Shan, J, and C.K. Toth, CRC Press, 2009.
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Increasing PRF
Multiple Pulses in Air "MPiA"
t0
Time , t0
The maximum range
(i.e., the range of thelast return) and the
PRF of the LiDAR
system are related
as,
T PRF
=
1
PRF
=
2"Rmax
v
Thus as an aircraft
flies at higher
altitude for large
area surveys, the PRF(and hence the
sampling density)must decrease.Announced in 2006 and commercially fielded in 2007,
MPiA is now a mainstream LiDAR technology.
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Interleaving Pulses-1
Region of
Interest
Region of ?
0
Rc
Rg
R
a n g e
Aircraft
For an aircraft high above theground at an altitude of ~1000
m may only be interested in
the ~100 m above the ground
“the region of interest”.
The air between the ground
and the region of interest
yields no significant echoes.
Is it possible to transmit
multiple pulses spaced suchthat their echoes do not
interfere with each other.
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Interleaving Pulses-2
0 tc tg
Recieved
Signal
0 tc tg
Recieved
Signal
T P R F
t c + T P R F
Pulse #1
Pulse #1 Pulse #2 Pulse #3
t g+ T P R F
2
x T P
R F
t c + 2
x T P R F
t g+ 2
x T P R F
The time from 0 to tc is“dead time”, while the
signal of interest is foundbetween tc and tg.
In a single pulse system thesecond pulse must await thereturn of the first pulse.
In an interleaved systemthe second pulse istransmitted “early” so thatit can return just after thefirst pulse without waiting
for tc.
Thus the PRF can bedoubled and possibly betripled or more.
0 tc tg
Recieved
Signal
Pulse #1 Pulse #2 Pulse #3
T P R F
t c
+ T P R F
t g
+ T P R F
2
x T P R F
t c + 2
x T P R F
t g+ 2
x T P R F
Pulse #4
3
x T P R F
t c
+ 3
x T P R F
t g
+ 3
x
T P R F 4
x T P R F
t c + 4
x T P R F
t g + 4
x T P R F
Pulse #5
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MPiA Performance
The relationship between PRF and flightheight for the Leica ALS60 system.Very high PRFs can exceed thecapabilities of current lasers. Thus
multiple laser systems are used toachieve very high PRFs (e.g., ~400 kHz).
The point density at a PRF of 400 KHz isshown as a function of ground speed andflight height for the Reigl LMS-Q680iAt 400 kHz the maximum single pulse
range is 375 m. Thus there are 3 pulsesin the air when flying at 800 m.
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Current Airborne LiDAR Systems
Toth, C. K., LARS, 2010.
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Kenai LiDAR Mappingin 2008-1
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Kenai LiDAR Mapping in 2008-2
LiDAR mapping of the 4550 square miles (11,780 km2) of the Kenai Peninsula.
Kenai LiDAR Mapping
Location Western Lowlands Eastern Kenai Watershed
Area 3295 sq miles (8530 km2) 1255 sq miles (3250 km2)
Post Spacing 1.4 m 3.0 m
Horizontal Accuracy 1 m 2.0
BareEarth RMSE 18.5 cm 50 cm
• Contract to Aero-Metric for LiDAR data collection and processing.• Kenai Watershed Forum contract to Alaska Satellite Facility (ASF) at the Geophysical
Institute-University of Alaska Fairbanks (GI-UAF) to provide Quality Assurance.
ASF Quality Assurance included;1. Review of formatting and completeness of data deliverables2. Review of the completeness, clarity, and compliance of the metadata3. Review of the contractor-provided quality assurance reports4. Evaluation of the planimetric accuracy of the LiDAR data5. Evaluation of the height accuracy of the LiDAR data6. Identification and characterization of any systematic errors observed in the data
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Planimetric Assessment of Road Intersection from GI-UAF Geodetic Control
Courtesy Rick Guritz, ASF, GI-UAF.
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Planimetric Assessment of Lake Point from GI-UAFGeodetic Control
Courtesy Rick Guritz, ASF, GI-UAF.
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Alaskan LiDAR Mapping
Region of
Interest
0
Rg
R a n g e
GroundGround
Snow
Ground
Leaves
Early-April Late-April Early-May
In wooded terrain the trees may shadow the ground. A better ground map will be obtainedif the survey is conducted AFTER snow has melted and BEFORE trees have leafed out.
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LiDAR Researchers atUniversity of Alaska Fairbanks
Researcher Primary Focus Contact
Anthony Arendt Glacier Mapping [email protected] Collins Atmospheric Sciences [email protected] Cunningham Terrestrial Mapping [email protected]
Javier Fochesatto Atmospheric Sciences [email protected]
Rick Guritz Terrestrial Mapping [email protected] Sassen Atmospheric Sciences [email protected]
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Eruption of Mount Augustine in 2006
PUFF Model Forecast
Lidar Data
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Acknowledgements
LiDAR research at the University of Alaska Fairbanks has been conducted with
support from the following;• State of Alaska
• US Department of Agriculture
• US Department of Defense
• US Geological Survey
• US National Aeronautics and Space Administration
•
US National Oceanic and Atmospheric Administration• US National Science Foundation
• Government of Japan
• Fulbright Commission of Germany
LiDAR research at the University of Alaska Fairbanks depends on the active
participation of undergraduate and graduate students.
Thanks to Rick Guritz and Keith Cunningham for helpful discussions.