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Thesis - Leigh Moody.pdf - Bad Request - Cranfield University

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Chapter 3 / Sensors / Radar<br />

_ _<br />

S<br />

: =<br />

I<br />

S<br />

⋅ σ<br />

4 ⋅ π ⋅<br />

RCS<br />

2<br />

Po,<br />

t<br />

3.8-9<br />

: =<br />

P<br />

T<br />

⋅ G<br />

2<br />

⋅ λ<br />

2<br />

T<br />

⋅ σ<br />

3 4<br />

( 4 ⋅ π ) ⋅ P<br />

o,<br />

t<br />

RCS<br />

Equation 3.8-25<br />

For a circular Gaussian radiation pattern the directive gain is a function of<br />

the antenna beam width and the antenna efficiency (λE),<br />

G : = λ ⋅ π ξ<br />

E<br />

2<br />

2<br />

BW<br />

Equation 3.8-26<br />

The noise power (N) available for a single pulse at the perfect receiving<br />

antenna measured in (W/Hz),<br />

N : = k ⋅ T<br />

B<br />

S<br />

t<br />

P<br />

Equation 3.8-27<br />

(kB) is Boltzmann's constant, and (tP) the uncompressed transmitted pulse<br />

length which is a piecewise constant function of target range, a typical<br />

approximation being,<br />

t<br />

P<br />

: =<br />

0.<br />

0027<br />

⋅ P<br />

XT<br />

o,<br />

t<br />

The system noise temperature (TS) is the sum of,<br />

S<br />

A<br />

R<br />

1 x 10<br />

1 x 10<br />

T = T + T + L ⋅T<br />

R<br />

−4<br />

−6<br />

E<br />

Equation 3.8-28<br />

Equation 3.8-29<br />

(TA) is the antenna noise comprising atmospheric and ground components,<br />

T<br />

A<br />

: =<br />

9 ⋅ TTS<br />

+ T<br />

10 ⋅ L<br />

O<br />

O<br />

TO<br />

+<br />

1 + L<br />

O<br />

Equation 3.8-30<br />

(LO) is the antenna ohmic loss factor, and (TO) the ground temperature. The<br />

sky noise temperature (TTS) is a function of beam elevation with respect to<br />

the Alignment frame.<br />

Θ<br />

TB<br />

A<br />

<<br />

30 ⋅ π<br />

180<br />

⇒<br />

T<br />

TS<br />

: =<br />

9.<br />

3433<br />

+<br />

0.<br />

03715<br />

⋅<br />

Θ<br />

TB<br />

A<br />

Equation 3.8-31

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