02.04.2013 Views

SN User's Guide - ESC Home - NASA

SN User's Guide - ESC Home - NASA

SN User's Guide - ESC Home - NASA

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

d. After symbol/decoder and symbol/deinterleaver/decoder synchronization is<br />

achieved, MA return service channel data is available at the <strong>SN</strong> ground terminal<br />

interface.<br />

e. To minimize return data loss, it is recommended that the customer platform<br />

transmit idle pattern on its data channels until after it has observed (via the user<br />

performance data (UPD) data) that the <strong>SN</strong> ground terminal has completed all of<br />

its data channel signal acquisition processes.<br />

f. Requirements for bit error probability and symbol slipping take effect at the time<br />

decoder synchronization is achieved.<br />

NOTE:<br />

Acquisition times will be reduced when data and symbol<br />

transition density values are higher than the minimum<br />

required.<br />

5.3.3.2 Bit Error Rate (BER)<br />

Table 5-8 provides Prec equations that will result in a customer achieving a BER of 10 -5<br />

for TDRSS compatible signals. The BER Prec equations are applicable for either<br />

powered (SMAR only) or non-powered flight dynamics and the following conditions:<br />

a. Data Encoding. Convolutional encoding (rate 1/2 or rate 1/3 (SMAR only))<br />

should be used for all customer platform MA transmissions both to minimize Prec<br />

and as an RFI mitigation technique. Detailed coding design is described in<br />

Appendix B. Reed-Solomon decoding is available to WDISC customers; typical<br />

performance is given in Appendix K.<br />

NOTE:<br />

For all configurations and modes, the <strong>SN</strong> is capable of<br />

providing SMAR support of uncoded links; however,<br />

performance is not guaranteed in RFI and must be<br />

coordinated with GSFC Code 450.<br />

b. Received Power. Prec is in units of dBW. The customer project, in determining<br />

its design requirements for minimum customer spacecraft EIRP, must take into<br />

account customer platform transmit antenna pointing losses, the space loss<br />

between the customer platform and the TDRS, and the polarization loss<br />

incurred between the customer platform transmit antenna and the TDRS<br />

receive antenna. The maximum TDRS receive antenna axial ratio is given in<br />

Table 5-8 (also refer to Appendix A). For DG1 and DG2 services, the following<br />

conditions apply:<br />

1. Balanced Power Single Data Source-Identical Data on the I and Q<br />

Channels (DG1 mode 1 and 2 only). For a customer platform<br />

synchronously transmitting identical data on the I and Q channels (single<br />

data source – identical data) with a balanced I and Q channel power<br />

Revision 10 5-27 450-<strong>SN</strong>UG

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!