Downlink CNR (Carrier to noise ratio in satellite reception) is an important figure in system TVRO design. Below are certain parameters used in CNR computation.
Figure of merit is given as
f= | g |
t |
t=ta+(n-1) ⋅ t0
f= | g |
ta+(n-1) ⋅ t0 |
F=10 log10(f)
Path loss is defined as
l=(
4 ⋅ \pi ⋅ d | |
λ |
)2
Where
λ
L=20 log10\left(
4 ⋅ \pi ⋅ d | |
λ |
\right)
L=20 log10\left(
4 ⋅ \pi ⋅ d ⋅ f | |
c |
\right)
Where c is the velocity of light.
With metric units
L=-147.56+20 log10(d)+20 log10(f)
L=92.45+20 log10(d)+20 log10(f)
L=96.58+20 log10(d)+20 log10(f)
Pe is the Equivalent isotropically radiated power (also known as EIRP) in dBW. It depends on the output of the transponders of the satellite and the antenna gain of the transmitting antenna. This figure is given by the service provider.
Pe=10 log10(p)+10 log10(gt)
where p is the output power of the transponder and g is the antenna gain.
B is the baseband of the channel given in dB
B=10 log10(b)
When b is given in MHz, than
B=10 log10(b)+60
K is the Boltzmann constant given in dB units.
K=10 log10(1.380 ⋅ 10-23)=-228.6