Lecture 12: Curvature and Refraction Radar Equation for Point Targets (Rinehart Ch3-4)

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MET 4410 Remote Sensing: Radar and Satellite Meteorology MET 5412 Remote Sensing in Meteorology Lecture 12: Curvature and Refraction Radar Equation for Point Targets (Rinehart Ch3-4)

Radar Wave Propagation In the clear air without rain or cloud: Reflection & refraction Ø We can treat that the air as homogenous medium stratified into horizontal layers. The the radar EM waves are incident on a planar (flat) boundary between different layers. In this case, we can use reflection/refraction to understand how the radar wave is propagating in the atmosphere. In rain or cloud: we need to consider absorption & scattering by particles

Radar Wave Propagation In rain or cloud: scattering by particles Ø Negligible scattering regime: when particle size is much smaller than the wavelength. We only need to consider absorption Ø Optics regime: when particle size is much larger than the wavelength, we can use the laws of reflection & refraction Ø Rayleigh or Mie regime : when the wavelength is comparable to the particle size. For microwave band radar detecting cloud drops or raindrops, it falls into this regime, therefore, we have to consider scattering.

Radar wave propagation in the air: Curvature and Refraction Recall complex refractive index: N = n ni r i The real part n r controls the phase speed of the EM wave through the medium. n r is defined as the ratio of the speed of light in vacuum c to the speed of EM waves through the medium c 1 : n " = $ $ % For all real substance, n r >1. n r air 1.0003 to 1.0004 at visible band, at sea level

The real part of refractive index in the air n " is between 1.0003 to 1.0004 The EM radiation travels about 0.03% to 0.04% slower in the air than in a vacuum n " decreases from 1.0003 near surface of the Earth to 1.0000 at the top of the atmosphere: usually it s a gradual decrease, but there could be some abrupt changes. n " is important to understand the radar wave propagation in the atmosphere!

Refractivity: Refractivity N r = ( n 1) 10 When n " =1.0003, N r =300, which is a more convenient number Refractivity of the atmosphere is dependent upon pressure, temperature, and humidity. Radar wave propagation is more dependent upon the gradient of refractivity rather than the absolute value of refractivity at any point. r 6

-39

Snell s Law Under normal atmospheric conditions, refractivity is largest near the ground and decreases with height. Therefore, radar waves will travel faster aloft than near the surface. This bends the waves in a downward direction relative to the horizontal. Why? Snell s Law: sin θ ( n ) i r r sin θ = ( n ) = u u r r i r i

Less Dense Medium N smaller More Dense Medium N larger Earth s curvature effect: if there is no atmosphere on Earth, radar rays would travel in straight lines. The curvature of the Earth beneath the ray would gradually cause the ray to be higher and higher above the Earth farther and farther from the radar. Relative to the Earth, the radar wave would appear bend upward!

Radar Wave Propagation: Curvature Effect Curvature is the angular rate of change necessary to follow a curved path. The curvature C of a circle is thus the angular distance traversed divided by the linear distance traversed: C δθ 2π 1 = = = δs 2πR R Where R is the radius of the circle.

Curvature Therefore, the Earth s curvature is 1, R = 6374km R The curvature due to refraction in the atmosphere is dependent on the refractive index change with height: δ n r where is the real part of the refractive index, and H is the height. For standard refraction condition: δ n r δ H n r δ H = 39 10 km 6 1

Curvature Then the total curvature of radar rays due to both Earth curvature and standard atmospheric refraction is: δ n r 1 1 1 39 10 1.179 10 = + = = Rʹ R δ H 6374km km km Which is equivalent to: 6 4 Rʹ = 8483km 1.33 R (4 / 3) R The effective Earth radius Rʹ is a fictitious Earth s radius. Under standard refraction conditions, the radar rays travel along the curvature of this fictitious Earth s surface.

Standard Refraction (Radar book Fig 3.7)

Super Refraction/Ducting (Trapping) Super refraction happens when the downward bending of radar waves is stronger than normal. Super refraction occurs when temperature increases with height (inversion) Ducting (trapping) is exceptional super refraction when the radius of curvature for the wave becomes smaller than Earth s and the radar waves are trapped in a layer of the atmosphere. Ducting increases the radar detection range, but it also increases ground clutter.

Radar Equation for Point Targets Motivation: Beside locating storms, radars can also measure the strength of the returned power, therefore estimating rain rate and convective intensity, etc. Therefore, we must know how to use radar quantitatively.

Radar equation: Solving the radar received power from transmitted power Panel a: Radar power (unit: W) transmitted by an isotropic antenna Panel b: using a real antenna, the power at a point on the beam axis is increased by a factor of the antenna gain. Panel c: the power intercepted by a target with area A is reradiated isotropically in all directions, with some of it received back at the radar. Fig. 4.1

Radar Equation for Point Targets Assume the radar power is P t at radar s original location. For an isotropic antenna, the radar power density S (W/m 2 ) at range r from the radar is: P S = t 4π r 2 Then for a real antenna, it should be: S = Pg t 4π r 2

Radar Equation for Point Targets Then the power intercepted by the target at range r from the radar is: P σ = PgA t 4π r where A σ is the cross section area of the target. σ 2

Radar Equation for Point Targets Assume that power intercepted by the target is reradiated isotropically back into space, then the energy amount received back at the radar will be: PA PgAA P = σ e = t σ e r 4 πr 2 (4 πr 2 ) 2 where A e is the effective area of the receiving antenna: 2 gλ Ae = 4π

Radar Equation for Point Targets Substitute and get the radar equation for point target: Pg 2 λ 2 A P = t σ r 64π 3 r 4 Wait a minute, is this correct? -- No. In fact, because the physical size of the target is not necessarily the size the target interacts with (appears ) to the radar. Instead, we should use the backscattering cross-section σ to replace A σ. So the final radar equation is: P r = Pg t 2 2 λσ 3 4 64π r

Back Scattering Cross Section for Spherical Targets Optical region: valid for spheres larger than wavelength (x=πd/λ>10, D is the diameter, a is 2 the radius): Rayleigh regime: when the size of a sphere is small compared to the wavelength (x=π D/λ<0.1) where σ = σ = πa m π 5 2 6 K 4 λ 1, D 2 2 K = m= N 2 2 m + 2 N1 N 2 is the complex index of refraction of the sphere (target). N

How to derive Back Scattering Cross Section (Petty CH12) Recall Rayleigh solution (lec 10) scattering efficiency: Q ' = ( ) x+ K - Backscattering efficiency Q b is Q s at backward direction θ = π. Then for rayleigh phase function, Q 2 = 4x + K - Backscattering cross section: σ 2 = Q 2 πr - = 4x + K - πr - = 67 8 9 : ; where diameter D=2r, σ = σ 2 2 π K D σ = 4 λ 5 6 λ =

Back Scattering Cross Section: Mie Solution Y-axis: backscattering efficiency X-axis: size Parameter x

Back Scattering Cross Section In Rayleigh regime, the backscattering cross section is proportional to D 6 Mie regime (0.1< π D/λ<10): the backscattering cross section σ can decrease as the particle size increases for certain size parameters

Summary The combination effect of Earth curvature and atmosphere refraction causes the radar rays bend upward relative to the Earth surface under standard refraction condition. Super refraction may cause ducting. Rayleigh regime: σ ~ D 6 ; Optical regime: σ= geometric area; Mie regime: complicated