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(ATBD) SMAP Level 1 Radar Data Products - NASA

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46<br />

where P n is the internal thermal noise power. Ground processing will estimate the<br />

internal noise power using noise only measurements and subtract this from the raw<br />

signal+noise measurements. The resulting estimate of P s is subject to statistical<br />

error from both P sn and P n which is given by [10]<br />

K 2 pc = 1<br />

Nτ p B (1 + 2<br />

SNR + 1<br />

SNR 2 ) (40)<br />

where N is the number of pulses averaged together, τ p is the pulse width, and B is<br />

the measurement bandwidth.<br />

Both K pc and N vary as a function of scan position or cross-track position. K pc<br />

also varies as a function of SNR which depends on the scene being observed. The<br />

requirements are generally applied for the worst case position which is the inner<br />

edge of the usable swath for K pc , and assuming the average scene backscatter level<br />

matches the designated minimum σ 0 level of -25 dB. Figures 15 and 16 show the<br />

variation of looks (N) and K pc as functions of cross track distance. The inner edge<br />

of the usable swath occurs at 150 km cross track distance, while the outer edge lies<br />

at 500 km cross track distance. Additional details on these performance parameters<br />

and how they relate to requirements are available in a preliminary calibration report<br />

[7].<br />

9.4 <strong>Radar</strong> Equation and Error Budget<br />

The normalized backscattering cross-section σ 0 is related to the received power by<br />

the radar equation (Sec. 7.16, [8]),<br />

P s (t) =<br />

λ2 P t (t −<br />

(4π)<br />

∫A<br />

2R)u c rw(t)G 2 σ 0<br />

dA (41)<br />

3 R 4<br />

where P s (t) is the received signal power referenced at the antenna port at time t, λ is<br />

the transmitted wavelength, A is the area on the surface illuminated by the antenna<br />

main lobe, P t (t) is the radiated transmit power pulse train, urw(t) is the receive<br />

window filter, G is the antenna gain (neglecting transmit receive differences due to<br />

spacecraft motion during the round trip time), σ 0 is the normalized backscattering<br />

cross-section, and R is the range to the surface. The receive window filter is defined<br />

by<br />

{<br />

1 for τrwd < t < τ<br />

urw(t) =<br />

rwd + τrw<br />

(42)<br />

0 otherwise<br />

where τ rwd is the delay from the start of a transmitted pulse train to the time the<br />

receive window is opened and the receiver begins digitizing echo power, and τrw is<br />

the duration of the echo buffer.

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