Constraints and parameters for the system design » History » Version 2
AUGER, Anne sophie, 03/23/2015 09:54 AM
1 | 1 | GAY, Adrien | h1. Constraints and parameters for the system design |
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2 | 1 | GAY, Adrien | |
3 | 2 | AUGER, Anne sophie | * Required bit rate |
4 | 2 | AUGER, Anne sophie | |
5 | 2 | AUGER, Anne sophie | In order to define the bit rate required for the transmission of video streams we need some input parameters, provided in the mission statement: |
6 | 2 | AUGER, Anne sophie | # aspect ratio of the video : AR=1,78 |
7 | 2 | AUGER, Anne sophie | # quality of the encoded video L=720p |
8 | 2 | AUGER, Anne sophie | # frame cadence FPS=12 fps |
9 | 2 | AUGER, Anne sophie | |
10 | 2 | AUGER, Anne sophie | We used the following formula |
11 | 2 | AUGER, Anne sophie | |
12 | 2 | AUGER, Anne sophie | p=. Bit rate = FPS*5,0692 * L ^1,391^ /(1000*AR) |
13 | 2 | AUGER, Anne sophie | |
14 | 2 | AUGER, Anne sophie | So |
15 | 2 | AUGER, Anne sophie | |
16 | 2 | AUGER, Anne sophie | p=. *Bit rate=322 Kbps* |
17 | 2 | AUGER, Anne sophie | |
18 | 2 | AUGER, Anne sophie | 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. |
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20 | 2 | AUGER, Anne sophie | |
21 | 2 | AUGER, Anne sophie | |
22 | 1 | GAY, Adrien | # Network constraints |
23 | 1 | GAY, Adrien | |
24 | 1 | GAY, Adrien | > * Frame format |
25 | 1 | GAY, Adrien | |
26 | 1 | GAY, Adrien | The application foreseen aims at transmitting multimedia content (video on the downlink), so we choose to use the MPEG-4 coding standard. The associated frame format MP4 is particularly adapted for the encapsulation of multimedia data type. |
27 | 1 | GAY, Adrien | |
28 | 1 | GAY, Adrien | > * Protocol stack |
29 | 1 | GAY, Adrien | |
30 | 1 | GAY, Adrien | # Antenna choice |
31 | 1 | GAY, Adrien | |
32 | 1 | GAY, Adrien | > * On board antenna |
33 | 1 | GAY, Adrien | The antenna placed on the aircraft must be compliant with the flight constraints listed in the introduction. Indeed, we should maintain the communication link while the aircraft is performing a turn ( +/- 15° attitude), landing or taking off ( +/- 45° inclination). Therefore, he position of the antenna must be carefully determined in order to be at LOS. |
34 | 1 | GAY, Adrien | |
35 | 1 | GAY, Adrien | Another constraint is the embedded |
36 | 1 | GAY, Adrien | |
37 | 1 | GAY, Adrien | > * Ground station antenna |