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Radar Doppler Velocities

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1 Radar Doppler Velocities
Fundamentals of Doppler Radar Mesocyclone WER Hook Echo Radar Reflectivity Radar Doppler Velocities Atmospheric Instrumentation M. D. Eastin

2 Outline Fundamentals of Doppler Radar Basic Concept Single Radar Pulse
Multiple Radar Pulses Maximum Doppler Velocity Range Doppler Dilemma Doppler Spectra of Weather Targets Basic Interpretation of Doppler Velocities Dual-Doppler Radar Analysis Airborne Doppler Radar Analysis Atmospheric Instrumentation M. D. Eastin

3 Basic Concept Doppler Effect: Generic Definition
A frequency shift (cycles per second → Hertz) of any electromagnetic wave pulse due to the “target” moving toward or away from the observer Atmospheric Instrumentation M. D. Eastin

4 Basic Concept Doppler Effect: Sound Waves
The Doppler shift for sound waves is the change in sound that one hears as race cars or airplanes approach and then recede from a stationary observer Atmospheric Instrumentation M. D. Eastin

5 Basic Concept Doppler Effect: Meteorology
A frequency shift between the transmitted radar pulse and the return echo pulse due to hydrometeors moving either toward or away from the radar antenna Atmospheric Instrumentation M. D. Eastin

6 Doppler Frequency Shift
Single Radar Pulse Doppler Effect: Frequency Shift The relationship between the return echo frequency to the transmitted pulse frequency is: (1) where: fR = return echo frequency (s-1) fT = transmitted frequency (s-1) vR = “along-beam” radial velocity (m s-1) c = speed of light (m s-1) The frequency difference between the return echo and transmitted pulse (after a little algebra): (2) where: fDOP = Doppler frequency (s-1) Stationary Target Moving Away Doppler Frequency Shift Moving Toward Atmospheric Instrumentation M. D. Eastin

7 Single Radar Pulse Doppler Effect: Frequency Shift
Since the Doppler frequency shift is computed from the difference (or subtraction) between the transmitted and return echo frequencies, a radar must “listen” long enough (Δt) to observe a full waveform (0 → 2π) of the Doppler shift frequency If we assume: fT = 3 × 109 s-1 (10-cm radar) c = 3 × 108 m s-1 vR = 1 m s-1 (for minimum shift) Minimum Required Listening Time: Δt = 1.0 × 10-1 s Maximum Allowed Listening Time: TR = 1.0 × 10-3 s (pulse period of the WSR-88D) PROBLEM: The radar would need to “listen” at least 100 times longer between each pulse to observe the full waveform of the Doppler frequency shift Longer listening times require slower antenna rotation rates Single elevation: 30 minutes Single VCP: hours We must use another method !!! Not Practical Atmospheric Instrumentation M. D. Eastin

8 Single Radar Pulse Doppler Effect: Frequency Shift
Police officers are required to keep the radar “gun” focused on an individual vehicle for several seconds in order to obtain a full waveform of the Doppler shift frequency Atmospheric Instrumentation M. D. Eastin

9 Single Radar Pulse Doppler Effect: Phase Shift
The frequency difference can also be expressed as a phase shift (0 → 2π) between the return echo and the transmitted pulse (3) where: fDOP = Doppler frequency (s-1) fT = transmitted frequency (s-1) Δφ = phase shift (radians) Δt = elapsed time (s) c = speed of light (m s-1) If we use the relationship between transmitted frequency and wavelength, we can define the fractional phase shift for a single return echo: (4) π π/3 Time Amplitude Atmospheric Instrumentation M. D. Eastin

10 Transmitted Pulse Wavelength (λ)
Single Radar Pulse Doppler Effect: Phase Shift Magnitude Since we know the transmitted wavelength (λ), we can estimate the maximum fractional phase shift (Δφ/2π) of a single return echo using the pulse period (Δt = TR) for a typical range of Doppler radial velocities (vR) PROBLEM: As expected, the maximum fractional phase shift (Δφ/2π) returned by a single pulse is much smaller than the full phase shift cycle required to reconstruct the return echo “wave form” and determine the Doppler frequency Phase Shift (Δφ/2π) Transmitted Pulse Wavelength (λ) [ for TR = 1×10-3 s ] X-band C-band S-band Radial Velocity (vR) ( 3-cm ) ( 5-cm ) ( 10-cm ) 1 m/s 0.067 0.040 0.020 5 m/s 0.333 0.200 0.100 10 m/s 0.667 0.400 Atmospheric Instrumentation M. D. Eastin

11 Full Doppler Frequency Cycle
Multiple Radar Pulses Method to Overcome: Transmit a rapid-fire “train” of multiple pulses → increase the pulse repetition frequency Each pulse in the “train” will return a slightly different phase (φ1, φ2, φ3, φ4, … φN) The multiple phase shifts are used to reconstruct (estimate) the full Doppler shift cycle Doppler radial velocity (vR) is then computed from the mean phase shift along the train Full Doppler Frequency Cycle Time Phase shift from a single pulse in a pulse train Amplitude Atmospheric Instrumentation M. D. Eastin

12 Multiple Radar Pulses ANOTHER PROBLEM No unique solution
More than one Doppler frequency (or waveform) will “fit” a finite sample of phase shifts Minimum Phase Criteria: A minimum of two phase observations are required to determine a waveform of a Doppler frequency (N ≥ 2) OR The phase change between any two successive pulses must be less than half a wavelength (Δφ ≤ π) Other Criteria: Since the maximum number of phase observations is set by the pulse repetition frequency and the minimum number is set by the wavelength, there is a range of possible radial velocities than can be unambiguously determined (next few slides…) Time Amplitude Atmospheric Instrumentation M. D. Eastin

13 Maximum Radial Velocity Range
Nyquist Velocity: Starting with (4) and using the pulse period (TR) – or time between sequential pulses – for the maximum elapsed time (Δt): (5) We next re-arrange and apply the “half wavelength criteria” (0 → π) OR (6) Solving (6) for radial velocity (vR) and using the relationship between pulse period (TR) and pulse repetition frequency (F) (7) The Nyquist velocity represents the maximum (or minimum) radial velocity a Doppler radar can measure unambiguously [ function of wavelength and pulse repetition frequency ] Atmospheric Instrumentation M. D. Eastin

14 Unambiguous Velocity Range Actual Radial Velocity
Maximum Radial Velocity Range Nyquist Velocity: The maximum (or minimum) radial velocity a radar can measure unambiguously Any actual radial velocities larger (or smaller) than this value will be “aliased” back into another unambiguous range → multiple aliases can occur Example: Assume a radar with a Nyquist velocity of ±10 m/s observes an area of rainfall moving away from the radar at 15 m/s [ Reported Actual ] Aliased Velocities -10 10 -5 5 Unambiguous Velocity Range -20 -30 20 30 Actual Radial Velocity Atmospheric Instrumentation M. D. Eastin

15 Radar Reflectivity (DBZ)
Maximum Radial Velocity Range Can you find the aliased velocities in this image? Radar Reflectivity (DBZ) Radial Velocity (VR) Atmospheric Instrumentation M. D. Eastin

16 They are inversely related
Doppler Dilemma Maximizing the Nyquist Velocity: This table shows that Doppler radars capable of measuring a large range of radial velocities unambiguously have a longer wavelength (λ) and a large pulse repetition frequency (F) Problem: Recall that in order for radars to maximize their range, a small pulse repetition frequency is required Nyquist Velocity Pulse Repetition Frequency (F) Wavelength (λ) 200 s-1 500 s-1 1000 s-1 2000 s-1 3 cm 1.5 3.75 7.5 15.0 5 cm 2.5 6.25 12.5 25.0 10 cm 5.0 50.0 Which do we choose? They are inversely related Atmospheric Instrumentation M. D. Eastin

17 Doppler Dilemma Maximizing the Nyquist Velocity:
Atmospheric Instrumentation M. D. Eastin

18 Measure radial velocity
Doppler Dilemma How to Circumvent the Dilemma: Radar transmits pulses at alternating low and high pulse repetition frequencies Lower frequencies are used for surveillance (reflectivity) Higher frequencies are used for velocities (radial winds) A version of this technique has been used regularly by the WSR-88D radars 1992–2008 → Alternating pulse repetition frequencies (lower two elevations scans) → Doppler winds determined out to 120 km range → Reflectivity determined out to 240 km range 2008–now → Separate lower elevation scans (different pulse repetition frequencies) → Doppler winds determined out to 300 km range → Reflectivity determined out to 360 km range Measure reflectivity Measure radial velocity Pulse Time Atmospheric Instrumentation M. D. Eastin

19 Doppler Dilemma Impact of the Dilemma:
The impact of determining radial velocities at a closer range than the radar reflectivity is the “purple haze” (or range folding) often seen at far ranges on Doppler radar imagery This results from echoes returning after the next pulse is transmitted (i.e., r > rMAX) Atmospheric Instrumentation M. D. Eastin

20 Doppler Spectra of Weather Targets
Variations in Radial Velocity: A series of rapid-fire pulses in a pulse train will measure a “spectrum” of Doppler frequencies (or radial velocities) from a which a “mean” and “standard deviation” can be computed Radial velocity (vR) = mean value of the spectrum Spectral width (σ) = standard deviation of the spectrum = measure of the “spread” in velocities observed within the sampling volume –VMAX +VMAX VR σ spectrum Atmospheric Instrumentation M. D. Eastin

21 Doppler Spectra of Weather Targets
Variations in Radial Velocity: Despite short time periods between each pulse of a rapid-fire pulse train, variations in the computed mean radial velocities exist due to (1) changes in air motions, and (2) variability in the drop size distribution within the contributing volume Reasons for Variability: 1. Wind shear 2. Turbulence 3. Differential fall velocity 4. Antenna rotation 5. Curvature in the main lobe Atmospheric Instrumentation M. D. Eastin

22 Doppler Spectra of Weather Targets
Variations in Radial Velocity: Doppler spectra observed by a vertically pointing radar during passage of a winter storm with mixed-phase precipitation Notice how the spectra at individual heights vary by 1-2 m/s as a result of variable drop diameters and their associated fall speeds Archived Spectra: Full spectra observed by the WSR-88D radars are not archived due to the large amount of storage space required However, the spectral width is archived and used by forecasters to help identify: 1. Small tornadoes at far ranges 2. Intense turbulence that may impact aircraft operations Atmospheric Instrumentation M. D. Eastin

23 Basic Interpretation of Doppler Velocities
Radial Velocity: Along-Beam Motion The measured radial velocity is that portion of the actual 3-D wind vector oriented along the radar beam [ most radial velocities contain horizontal and vertical motions ] Any single radar only measures one component of the three dimensional wind vector, so to obtain a more practical estimate of two or three-dimensional flow: 1. Users must learn how to interpret single radar Doppler imagery (next lecture…) 2. Multiple Doppler radars can be used to “re-construct” the 3-D flow (next topic…) Actual Wind Radial component seen by radar RADAR Atmospheric Instrumentation M. D. Eastin

24 Basic Interpretation of Doppler Velocities
Doppler Effect: Meteorology The sign [ + / – ] of the frequency shift is used to determine the color of the radial velocity data plotted on Doppler velocity displays A negative shift (called a “red shift” in optics) occurs as targets move away from the radar Lower frequency = Positive radial velocity = Outbound flow A positive shift (called a “green shift” in optics) occurs as targets move toward the radar Higher frequency = Negative radial velocity = Inbound flow These “color” shift conventions are then translated to radar displays: Red: Moving away from radar Green: Moving toward radar Atmospheric Instrumentation M. D. Eastin

25 Basic Interpretation of Doppler Velocities
Doppler Effect: Meteorology The magnitude of the frequency shift is used to determine the brightness of the radial velocity data plotted on Doppler velocity displays Much lower frequency = Strong outbound flow Slightly lower frequency = Weak outbound flow Much higher frequency = Strong inbound flow Slightly higher frequency = Weak inbound flow Atmospheric Instrumentation M. D. Eastin

26 Basic Interpretation of Doppler Velocities
Examples of Data from a Single Doppler Radar: GR2Analyst Demonstration Atmospheric Instrumentation M. D. Eastin

27 Dual-Doppler Radar Analysis
Using Two Doppler Radars: One of the key limitations of Doppler radar data is that it only measures one component of the three-dimensional (3-D) wind field However, if a second unique component of the same wind field can be measured, then the the third component can be derived (computed) using “boundary conditions” The second component should be observed at an angle 30°-90° different Requires the two radars to be “carefully spaced relative to one another” Atmospheric Instrumentation M. D. Eastin

28 Dual-Doppler Radar Analysis
Using Two Doppler Radars: The baseline distance between the two radars must be “small” in order to provide sufficient horizontal resolution (< 2 km) and coverage of the low-level (< 1 km) winds to observe the critical flow fields associated with any convective feature of interest [ Remember: Radar pulses expand in size and increase altitude far from the radar ] Baseline distances: Less than 100 km [ too far apart for WSR-88Ds ] [ easy for mobile DOWs ] Atmospheric Instrumentation M. D. Eastin

29 Dual-Doppler Radar Analysis
Doppler on Wheels (DOWs): Must be deployed (and leveled) within 10 km of the target storm Scans at multiple elevation angles or uses pre-programmed volume coverage patterns Alternates staggered pulse repetition frequencies for reflectivity and radial velocity measurements Can now operate in single or dual polarization modes Parameter DOW-1 DOW-2 Frequency 9.37 GHz 9.38 GHz Wavelength 3.2 cm (X-band) Radial resolution 12 m (minimum) Maximum PRF 3200 s-1 5000 s-1 Transmitted power 250 kW Pulse duration 2.0 μs Beam width 0.93° Gain 35 dB Rotation period 12 s 9 s Maximum Range 45 km 30 km Atmospheric Instrumentation M. D. Eastin

30 Dual-Doppler Radar Analysis
Doppler on Wheels (DOWs): During tornado chase field experiments, the DOW radars will carefully place themselves near a “promising” storm in order to collect dual-Doppler winds of the supercell and any tornado DOW-2 DOW-1 Atmospheric Instrumentation M. D. Eastin

31 Dual-Doppler Radar Analysis
Reconstructing 3-D Wind Fields: The two radars obtain two unique (nearly simultaneous) measurements of radar-relative “radial winds” across the dual-Doppler domain 1. The radial winds (vR1 and vR2) are used to derive the east-west (U) and north-south (V) horizontal wind components via → the radial winds are largely horizontal where: θ1 = elevation angle (degrees) of radar #1 θ2 = elevation angle (degrees) of radar #2 β1 = azimuth (degrees) of radar #1 β2 = azimuth (degrees) of radar #2 Details are provided in Wurman (1994) and Jorgensen et al. (1996) Atmospheric Instrumentation M. D. Eastin

32 Dual-Doppler Radar Analysis
Reconstructing 3-D Wind Fields: The two radars obtain two unique (nearly simultaneous) measurements of radar-relative “radial winds” across the dual-Doppler domain 2. The horizontal winds (U, V) are then used to compute the vertical wind (W) using a density-weighted version of the continuity equation (below), assuming the vertical motion a the ground is zero (W = 0 at z = 0), and subtracting an estimate of the mean hydrometeor fall speed (WF) – derived from the mean radar reflectivity – from the total vertical velocity (WT) where: ρ = atmospheric density (kg m-3) WT = total vertical velocity (m s-1) WF = hydrometeor fall speed (m s-1) Details are provided in Wurman (1994) and Jorgensen et al. (1996) Atmospheric Instrumentation M. D. Eastin

33 Dual-Doppler Radar Analysis
An Example: From Wurman et al. (2007) Atmospheric Instrumentation M. D. Eastin

34 Dual-Doppler Radar Analysis
An Example: From Wurman et al. (2007) Atmospheric Instrumentation M. D. Eastin

35 Dual-Doppler Radar Analysis
An Example: From Wurman et al. (2007) Atmospheric Instrumentation M. D. Eastin

36 Airborne Doppler Radar Analysis
Airborne Radars: NOAA WP-3D and NCAR Electra NOAA Tail Doppler radar Single antenna with adjustable tilt Scans in “vertical” plane normal to the aircraft track NCAR Tail Doppler radars Two antenna fixed at 18.5° fore/aft Scans in “vertical” plane normal to the aircraft track Parameter NOAA (one antenna) NCAR (both antenna) Frequency 9.32 GHz 9.40 GHz Wavelength 3.2 cm (X-band) Radial resolution 125 m 150 m Maximum PRF 1600 s-1 2000 s-1 Transmitted power 60 kW 50 kW Pulse duration 0.5 μs 1.0 μs Beam width 1.5° 1.8° Gain 40.0 dB 38.7 dB Rotation period 6.0 s 5.5 s Maximum Range 93 km 70 km Atmospheric Instrumentation M. D. Eastin

37 Airborne Doppler Radar Analysis
Airborne Doppler Radars: Similar to ground-based Doppler radars, if at least two unique “views” of the same wind field can be obtained in a short period of time (simultaneously) by airborne Doppler radars, then the three-dimensional wind field can be derived The two views should be observed at different angles (30°-90° apart) Requires the aircraft to complete a specific flight path Single Aircraft – Vertical Plane Scanning Antenna rotates through plane at 90° to the flight track Aircraft must “box-off” target convection by flying adjacent leg over a short period, and then turn 90° and fly a second leg of similar length Two views within 15 minutes at typical aircraft speeds Permits a “pseudo” dual Doppler analysis Aircraft track Atmospheric Instrumentation M. D. Eastin

38 Airborne Doppler Radar Analysis
Airborne Doppler Radars: Similar to ground-based Doppler radars, if at least two unique “views” of the same wind field can be obtained in a short period of time (simultaneously) by airborne Doppler radars, then the three-dimensional wind field can be derived The two views should be observed at different angles (30°-90° apart) Requires the aircraft to complete a specific flight path Single Aircraft – Fore-Aft (FAST) Scanning Antenna alternates between a tilt of ~20° fore and ~20° aft in subsequent rotations Two views within 1-2 minutes at typical aircraft speeds Does not require aircraft to box-off convection Permits a “pseudo” dual-Doppler analysis with less concern for storm steadiness Atmospheric Instrumentation M. D. Eastin

39 Airborne Doppler Radar Analysis
Airborne Doppler Radars: Similar to ground-based Doppler radars, if at least two unique “views” of the same wind field can be obtained in a short period of time (simultaneously) by airborne Doppler radars, then the three-dimensional wind field can be derived The two views should be observed at different angles (30°-90° apart) Requires the aircraft to complete a specific flight path Single Aircraft – Fore-Aft (FAST) Scanning Antenna alternates between a tilt of ~20° fore and ~20° aft in subsequent rotations Two views within 1-2 minutes at typical aircraft speeds Does not require aircraft to box-off convection Permits a “pseudo” dual-Doppler analysis with less concern for storm steadiness Atmospheric Instrumentation M. D. Eastin

40 Airborne Doppler Radar Analysis
Removing Navigation and Return Echo Errors: The aircraft motion and orientation must be accounted for and removed Drift angle ± 20° Pitch angle ± 10° Roll angle ± 45° Vertical motion ± 20 m/s Horizontal motion m/s Return echo considerations that must be accounted for or removed Low-power noise Sea clutter Second-trip echoes Side-lobe contamination De-aliasing radial velocities Drift Atmospheric Instrumentation M. D. Eastin

41 Airborne Doppler Radar Analysis
Removing Navigation and Return Echo Errors: Raw Data Low-Power Noise Notice aircraft’s tilt Sea Clutter Second Trip Echo Radar Reflectivity Radial Velocity Atmospheric Instrumentation M. D. Eastin

42 Airborne Doppler Radar Analysis
Removing Navigation and Return Echo Errors: “Cleaned” Data Radar Reflectivity Radial Velocity Atmospheric Instrumentation M. D. Eastin

43 Airborne Doppler Radar Analysis
Reconstructing 3-D Wind Fields: Similar to ground based-Doppler radars, the two radar views obtain two unique (nearly simultaneous) measurements of radar-relative “radial winds” within / near a given target 1. The radial winds (vR1 and vR2) are used to derive the east-west (U) and north-south (V) horizontal wind components where: θ1 = elevation angle (degrees) of radar #1 θ2 = elevation angle (degrees) of radar #2 β1 = azimuth (degrees) of radar #1 β2 = azimuth (degrees) of radar #2 Details are provided in Wurman (1994) and Jorgensen et al. (1996) Atmospheric Instrumentation M. D. Eastin

44 Airborne Doppler Radar Analysis
Reconstructing 3-D Wind Fields: Similar to ground based-Doppler radars, the two radar views obtain two unique (nearly simultaneous) measurements of radar-relative “radial winds” within / near a given target 2. The horizontal winds (U, V) are then used to compute the vertical wind (W) using a density-weighted version of the continuity equation (below), assuming the vertical motion a the ground is zero (W = 0 at z = 0), and subtracting an estimate of the mean hydrometeor fall speed (WF) – derived from the mean radar reflectivity – from the observed total vertical velocity (WT) where: ρ = atmospheric density (kg m-3) WT = total vertical velocity (m s-1) WF = hydrometeor fall speed (m s-1) Details are provided in Wurman (1994) and Jorgensen et al. (1996) Atmospheric Instrumentation M. D. Eastin

45 Dual-Doppler Analysis
Airborne Doppler Radar Analysis An Example: Aircraft Pass #2 Pass #1 “Pseudo” Dual-Doppler Analysis A B Winds Reflectivity z = 3.5 km Atmospheric Instrumentation M. D. Eastin

46 Airborne Doppler Radar Analysis
An Example: A B Atmospheric Instrumentation M. D. Eastin

47 Summary Fundamentals of Doppler Radar Basic Concept Single Radar Pulse
Multiple Radar Pulses Maximum Doppler Velocity Range Doppler Dilemma Doppler Spectra of Weather Targets Basic Interpretation of Doppler Velocities Dual-Doppler Radar Analysis Airborne Doppler Radar Analysis Atmospheric Instrumentation M. D. Eastin

48 References Atmospheric Instrumentation M. D. Eastin
Atlas , D., 1990: Radar in Meteorology, American Meteorological Society, 806 pp. Crum, T. D., R. L. Alberty, and D. W. Burgess, 1993: Recording, archiving, and using WSR-88D data. Bulletin of the American Meteorological Society, 74, Doviak, R. J., and D. S. Zrnic, 1993: Doppler Radar and Weather Observations, Academic Press, 320 pp. Fabry, F., 2015: Radar Meteorology Principles and Practice, Cambridge University Press, 256 pp. Joregensen, D. P., T. Matejka, and J. D. DuGranrut, 1996: Multi-beam techniques for deriving wind fields from airborne Doppler radars. Meteorology and Atmospheric Physics, 59, Lee, W. C., F. D. Marks, and C. Walther, 2003: Airborne Doppler radar analysis workshop. Bulletin of the American Meteorological Society, 84, Reinhart, R. E., 2004: Radar for Meteorologists, Wiley- Blackwell Publishing, 250 pp. Wurman, J. 1994: vector winds from a single-transmitter bistatic dual-Doppler radar network. Bulletin of the American Meteorological Society, 75, Wurman, J, Y. Richardson, C. Alexander, S. Weygandt, and P. F Zhang, 2007: Dual-Doppler analysis of winds and vorticity budget terms near a tornado. Monthly Weather Review, 135, Atmospheric Instrumentation M. D. Eastin


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