Constraints for the physical layer and RF equipment » History » Version 4
Version 3 (GAY, Adrien, 03/24/2015 12:31 AM) → Version 4/6 (GAY, Adrien, 03/24/2015 12:35 AM)
h1. Constraints for the physical layer and RF equipment
h2. Constraints for the physical layer and RF equipment:
* Required bit rate
In order to define the bit rate required for the transmission of video streams we need some input parameters, provided in the mission statement:
> # aspect ratio of the video : AR=1,78
> # quality of the encoded video L=720p
> # frame cadence FPS=12 fps
We used the following formula
p=. Bit rate = FPS*5,0692 * L ^1,391^ /(1000*AR)
So
p=. *Bit rate=322 Kbps*
As the link will allow video transmission, we will need an adapted encapsulation protocol, so we must take into account extra bits: we decide to define a bit rate of 500 kbps.
From the given allocated frequency band, the following parameters are defined:
* f : Central frequency of the emitted signal
* B: Width of the allocated bandwidth
* EIRP: Maximum power that can be emitted in a given direction
From the specifications, the following parameters are defined:
* Rb: Useful bit rate of the transmission
* R : Minimal distance for the transmission
The value of these parameters constrain the parameters of the physical layer and the RF equipment for the design of the system.
h3. Physical layer:
The study of the physical layer will be limited to the choice of the modulation, the coding and the shaping filter. We will consider a SRRC filter (Square Root Raised Cosine) for the shaping filter as it is commonly used in telecommunication systems for its good performances.
Then, the parameters of the physical layer are:
* M : Modulation (M=4 : QPSK, M=8 : 8PSK etc)
* rho : Coding rate (rho <1)
* alpha : roll-off of the SRRC filter
In fact all these parameters are linked through the spectral efficiency T of the system, which is fixed by B and Rb:
p=. $\tau = \frac{R_{b}}{B}$ and $\tau =\frac{\log_{2}(M)\rho}{1+\alpha}$
Then, the parameters of the physical have to comply with the following relation:
p=. $\frac{\log_{2}(M)\rho}{1+\alpha}>\frac{R_{b}}{B}$ T>cst
h3. Link budget:
Here is the expression of the link budget:
(link budget)
We can notice that all the parameters are already known, except:
* (G/T): Figure of merit of the receiver (ISAE antenna)
* Lmarg: Margin on the link budget to take into account all the perturbations (antenna
depointing, atmosphere attenuation, interferences, non-ideal demodulator …)
Lmarg being only linked to physical parameters, we don’t have any influence on it. Then, it has to be evaluated but it is not really a parameter of the design.
Power amplifier
h2. Conclusion:
From these considerations, our aim will be to:
* Choose the modulation and the coding (according to the shaping filter)
* Compute the gain of the receiving antenna
* Propose some technical solution for the receiving antenna
We will also develop tools to visualize the influence of the bandwidth, EIRP, useful bit rate and distance on the system design.
The aircraft antenna will be considered able to fulfil the required antenna pattern, but we will not discuss about technical solutions for this antenna, as it can be really tricky.
h2. Constraints for the physical layer and RF equipment:
* Required bit rate
In order to define the bit rate required for the transmission of video streams we need some input parameters, provided in the mission statement:
> # aspect ratio of the video : AR=1,78
> # quality of the encoded video L=720p
> # frame cadence FPS=12 fps
We used the following formula
p=. Bit rate = FPS*5,0692 * L ^1,391^ /(1000*AR)
So
p=. *Bit rate=322 Kbps*
As the link will allow video transmission, we will need an adapted encapsulation protocol, so we must take into account extra bits: we decide to define a bit rate of 500 kbps.
From the given allocated frequency band, the following parameters are defined:
* f : Central frequency of the emitted signal
* B: Width of the allocated bandwidth
* EIRP: Maximum power that can be emitted in a given direction
From the specifications, the following parameters are defined:
* Rb: Useful bit rate of the transmission
* R : Minimal distance for the transmission
The value of these parameters constrain the parameters of the physical layer and the RF equipment for the design of the system.
h3. Physical layer:
The study of the physical layer will be limited to the choice of the modulation, the coding and the shaping filter. We will consider a SRRC filter (Square Root Raised Cosine) for the shaping filter as it is commonly used in telecommunication systems for its good performances.
Then, the parameters of the physical layer are:
* M : Modulation (M=4 : QPSK, M=8 : 8PSK etc)
* rho : Coding rate (rho <1)
* alpha : roll-off of the SRRC filter
In fact all these parameters are linked through the spectral efficiency T of the system, which is fixed by B and Rb:
p=. $\tau = \frac{R_{b}}{B}$ and $\tau =\frac{\log_{2}(M)\rho}{1+\alpha}$
Then, the parameters of the physical have to comply with the following relation:
p=. $\frac{\log_{2}(M)\rho}{1+\alpha}>\frac{R_{b}}{B}$ T>cst
h3. Link budget:
Here is the expression of the link budget:
(link budget)
We can notice that all the parameters are already known, except:
* (G/T): Figure of merit of the receiver (ISAE antenna)
* Lmarg: Margin on the link budget to take into account all the perturbations (antenna
depointing, atmosphere attenuation, interferences, non-ideal demodulator …)
Lmarg being only linked to physical parameters, we don’t have any influence on it. Then, it has to be evaluated but it is not really a parameter of the design.
Power amplifier
h2. Conclusion:
From these considerations, our aim will be to:
* Choose the modulation and the coding (according to the shaping filter)
* Compute the gain of the receiving antenna
* Propose some technical solution for the receiving antenna
We will also develop tools to visualize the influence of the bandwidth, EIRP, useful bit rate and distance on the system design.
The aircraft antenna will be considered able to fulfil the required antenna pattern, but we will not discuss about technical solutions for this antenna, as it can be really tricky.