Aero 250 Equations Flashcards

1
Q

SNR(dB)

A

10log(Ps/Pn)

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2
Q

Modulation factor, mu

A

KaAm = Am/m

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3
Q

Channel capacity, C

A

BcLog2(1 + SNR) = BcLog(P/BcN0)

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4
Q

Carrier power, Pc

A

(Ac^2)/2

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5
Q

Angle modulated signal power, P

A

(A^2)/2

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6
Q

Carson’s rule

A

Banglemod = 2(B + ∆f) = 2B(ß + 1), where ß = ∆f/B

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7
Q

Sampling frequency, fs

A

1/Ts

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8
Q

Bit number, N

A

Log2(L), where L is the quantisation level.

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9
Q

Range, R

A

0.5ct, where t is transit time.

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10
Q

Range resolution, ∆R

A

c/2Bp, where Bp is the pulse bandwidth

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11
Q

Pulse bandwidth, Bp

A

1/Tp, where Tp is the pulse duration

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12
Q

Duty cycle, d

A

Tp/Tpri, where Tpri is the pulse repetition interval.

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13
Q

Max range, Rmax

A

c/2fprf, where fprf is the pulse repetition frequency.

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14
Q

Average power (radar)

A

dPpeak, where Ppeak is the peak power.

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15
Q

SNRintegrated

A

GI SNRperpulse

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16
Q

Beamwidth, ∆theta

A

1.22lambda/2a, where a is the radius of the circular aperture.

17
Q

Cross range resolution, ∆Rc

A

2RSin(∆theta/2)

18
Q

Range accuracy, sigmaR

A

∆R/√(2SNR) = c/2Bp√(2SNR)

19
Q

Angular accuracy, sigmaA

A

∆theta/1.6√(2SNR)

20
Q

Doppler shift, fd

A

2Vr/lambda, where Vr is the radial velocity

21
Q

Integration time for two doppler shifts, Tint

A

1/∆fd

22
Q

Doppler shift error, sigmafd

A

∆fd/√(2SNR)

23
Q

Radial velocity error, sigmaVr

A

lambda∆fd/2√(2SNR)

24
Q

Rayleigh criterion

A

∆theta = 1.22lambda/D

25
Q

Angular resolution, ∆theta

A

theta/N

26
Q

Noise power, N

A

kT0BF, where T0 is the temperature of the electronics, and F is the noise figure of the electronics.

27
Q

Antenna gain, G

A

4π/(∆theta)^2