prepared by j. rothermel* and s.c. johnson (nasa msfc) p.a. kromis (computer science corporation)

14
MSFC/GHCC 1 2 micron pulsed ground based lidar Non-Contact Velocity Measurements on Simulated River Surfaces Using Coherent Doppler Lidar Preliminary Results Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation) Earth Science Department NASA Marshall Space Flight Center Updated by D. Bowdle** (University of Alabama in Huntsville) [email protected] **[email protected]

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Non-Contact Velocity Measurements on Simulated River Surfaces Using Coherent Doppler Lidar Preliminary Results. Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation) Earth Science Department NASA Marshall Space Flight Center - PowerPoint PPT Presentation

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Page 1: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

12 micron pulsed ground based lidar

Non-Contact Velocity Measurementson Simulated River Surfaces

Using Coherent Doppler LidarPreliminary Results

Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC)P.A. Kromis (Computer Science Corporation)

Earth Science DepartmentNASA Marshall Space Flight Center

Updated by D. Bowdle** (University of Alabama in Huntsville)

[email protected] **[email protected]

Page 2: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

22 micron pulsed ground based lidar

MSFC Coherent Doppler Wind Lidar Initiated April 1999 Purpose:

CDWL technology validationAtmospheric properties researchSpace CDWL concepts investigationCDWL targets researchStudent Instruction

Location:MSFC Building 4467GSFC van (proposed)Van or trailer (future)Aircraft (future)

Initial components:Transceiver, 50 mJ, 6.6 Hz, 2.017 microns, FL pumped10 cm telescope from Schwartz Electro-Optics, Inc.Full hemispheric scanner (Bldg. 4467)Data acquisition & processing

Page 3: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

32 micron pulsed ground based lidar

Long-term Objective

Streamflow Measurement with Doppler Lidar Complement proposed microwave radar measurements Relationship among surface velocity profile, bottom topography, and discharge Based on phased approach Controlled experimental conditions (initial phase) Collaborations with USGS, U. Washington (later phases)

Doppler lidar is only technique that can directlymeasure the influence of near-surface winds

Page 4: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

42 micron pulsed ground based lidar

Background

Water surface velocity measurements depend on: Lidar wavelength Surface roughness Incidence (or nadir) angle Turbidity Surface contaminants (e.g., foam) Depth of penetration (of order millimeters at 2 micron) Near-surface wind velocity

Page 5: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

52 micron pulsed ground based lidar

Target

TargetTarget

Lidar LidarLidar~3

50 m

rang

e

(Very) Preliminary Experiment at MSFC

Page 6: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

62 micron pulsed ground based lidar

Water Slide Geometry

Water slide Nadir Angle

SlitWater Flow

Lidar Beam

Page 7: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

72 micron pulsed ground based lidar

Experiment Parameters MSFC Doppler lidar, 6.6 Hz, 2.017 m Velocities toward lidar are negative (-) Water discharge nozzles: weirgate on new waterslide Water slide surface composition: plexiglass Lidar beam footprint: ~10 cm Discharge depth: several mm (variable) Nadir angles at target: 30, 60 deg Integration: 20 pulses Range gate, velocity plots: 210 m, centered on target Range gate, range plots: 38.4 meters Range to target: ~350 meters Minimum range: ~150 meters Number of good range gates in air near target: ~5

Page 8: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

82 micron pulsed ground based lidar

LEGENDSide rails 2x43/4” p.t. plywd sheetPlate 2x4 Pipe (1-1/4” hvy ga. lined)Suspension tower 2x4Angle iron 1-?”Polycarbonate ?”Aircraft cableBolt

Plan ViewSide View NOTES:

1. Screws--No nails!2. HVHC plywood3. Pres. treated wood4. Zinc coated or

stainless h/w

Guides (polycarb)

Gate (polycarb)

Stick handle

Graduated adjustable stop (wing nut)

Turnbuckle (4)

Water

Capture plate (2)

16” width2’ 3” CL

Water

BeamApproximate

beam footprintduring operation

Open topWaterinlet

Carpet runner

MSFC Water Slide - Version 1.0J. Rothermel/NASA and D.A. Bowdle/UAH

Failsafe line

Page 9: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

92 micron pulsed ground based lidar

NOTES:1. No nails!2. Clear p.t. pine3. Level with blocks4. Level at 4 corners

LEGENDExternal frameMending platePlate 2x4; block 4x4 Pipe (1-1/4” hvy ga. lined)Brace 2x4Capture plateAircraft cableBolts

Plan View

Side View

Winchw/ lock Pulley

RetainerSlide outline

(horizontal position)

To slide

CL

Setscrew

BeamFailsafe line

Failsafe line

Carabiner

Page 10: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

102 micron pulsed ground based lidar

0 20 40 60 80 100 120 140 160 180 200

-4

-3

-2

-1

0

1

2

shot

m

e

t

e

r

s

/

s

e

c

o

n

d

Velocity vs. Shot

Figure 1 – Run 2, 210 Meter Range Gate Centered on Water Target, 30Degree Target Angle, Raw Target PSD Amplitude Threshold – 500,

Raw Target PSD Frequency Window – 750:850

Page 11: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

112 micron pulsed ground based lidar

0 20 40 60 80 100 120 140 160

-2.8

-2.6

-2.4

-2.2

-2

-1.8

-1.6

-1.4

-1.2

-1

shot

m

e

t

e

r

s

/

s

e

c

o

n

d

Velocity vs. Shot

Figure 2 - Run 3, 210 Meter Range Gate Centered on Water Target, 60Degree Target Angle, Raw Target PSD Amplitude Threshold – 500,

Raw Target PSD Frequency Window – 750:850

Page 12: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

122 micron pulsed ground based lidar

0 20 40 60 80 100 120 140 160 180 200

-0.8

-0.6

-0.4

-0.2

0

0.2

0.4

0.6

0.8

shot

m

e

t

e

r

s

/

s

e

c

o

n

d

Velocity vs. Shot

Figure 1 - Run 5, 210 Meter Range Gate Centered on Dry Target, 60Degree Target Angle, Raw Target PSD Amplitude Threshold – 500,

Raw Target PSD Frequency Window – 750:850

Page 13: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

132 micron pulsed ground based lidar

-0.8 -0.6 -0.4 -0.2 0 0.2 0.4 0.6 0.80

10

20

30

40

50

60

70

80

meters/second

shots

Shots vs. Velocity

Figure 1 - Run 5, 210 Meter Range Gate Centered on Dry Target, 60 Degree Target Angle, Raw Target PSD Amplitude Threshold – 500,

Raw Target PSD Frequency Window – 750:850

Page 14: Prepared by J. Rothermel* and S.C. Johnson (NASA MSFC) P.A. Kromis (Computer Science Corporation)

MSFC/GHCC

142 micron pulsed ground based lidar

Conclusions and Plans Conclusions

Velocity standard deviation for hard target is ~0.1 m/s. Velocity decreases slowly as reservoir empties, allows integrationSurface tension effects from untreated plexiglass slide surface create

flow channeling, with variable water layer thickness non-riverine water surface microstructure

Sanding the plexiglass surface reduces surface tension effectsvirtually eliminates flow channelingnearly mirror smooth water surfaces

PlansResume lidar operations (after minor repairs)Test runs with variable flow velocity and layer thicknessTest runs with controlled surface condition