written 8.5 years ago by | • modified 8.5 years ago |
This question appears in Mumbai University > Satellite Communication and Network subject
Marks: 6 M
Year: May 2015
written 8.5 years ago by | • modified 8.5 years ago |
This question appears in Mumbai University > Satellite Communication and Network subject
Marks: 6 M
Year: May 2015
written 8.5 years ago by |
A measure of the performance of a satellite link is the ratio of carrier power to noise power at the receiver input, and link-budget calculations are often concerned with determining this ratio.
Conventionally, the ratio is denoted by $\frac{C}{N}$ (or CNR), which is equivalent to $\frac{P_R}{P_N}$ . In terms of decibels,
$\frac{C}{N}=(P_R )-(P_N ) (1)$
Evaluating the values for $\frac{P_R}{P_N}$ , we get
$\frac{C}{N}=(EIRP)+(G_R )-(LOSSES)-(k)-(T_S )-(B_N) (2)$
The $\frac{G}{T}$ ratio is a key parameter in specifying the receiving system performance. The antenna gain $G_R$ and the system noise temperature $T_S$ can be combined in eq. (2) as
$[\frac{G}{T}]=[G_R ]-[T_S ]dBK^- (3)$
Therefore, the link equation becomes
$\frac{C}{N}=(EIRP)+(\frac{G}{T})-(LOSSES)-(k)-(T_S )-(B_N) (4)$
The ratio of carrier power to noise power density $\frac{P_R}{N_0}$may be the quantity actually required.
Since $P_N=kT_N B_N=N_0 B_N$, then
$[\frac{C}{N}]=[\frac{C}{N_0 B_N }]$
$= [\frac{C}{N_0 }]-[B_N ]$
…and therefore,
$[\frac{C}{N_0} ]=[\frac{C}{N}]+[B_N ] (5)$
$\frac{C}{N}$ is a true power ratio in units of decibels, and $B_N$ is in decibels relative to 1 Hz, or dBHz. Thus, the units for $[\frac{C}{N_0} ]$ are dBHz. Substituting eq. (5) for $[\frac{C}{N}]$ gives
$\frac{C}{N_0} =(EIRP)+(\frac{G}{T})-(LOSSES)-(k) (6)$