Aerospace and Electronic Systems Magazine June 2017 - 14
State-of-the-Art Space Mission Telecommand Receivers
Table 6.
Main Outcomes and Design Guidelines Resulting from the Study
Acquisition and Tracking
Critical issues due to very low SNR values discussed. Most
appropriate carrier, subcarrier and symbol tracking techniques
addressed, depending on mission scenarios.
Frame synchronization
Need to lengthen the start sequence up to 64 bits demonstrated.
Most convenient low-complexity, but near optimal, methods for
pattern recognition identified for both start and tail sequence
recognition.
Decoder
Error rate performance of the best decoding algorithms for the new
codes properly addressed. Impact of quantization analyzed. Residual
Undetected Error Rate evaluated.
Hardware implementation considerations
Proper architecture described. Main bottlenecks in the current onboard architecture highlighted and suitable enhancements proposed
for circumventing them, particularly in the most severe DS scenario.
lelization can be exploited to carry out the large number of binary
operations needed.
CONCLUSIONS AND OUTLOOK
In this article, we presented a survey of next generation decoders
and receiver chain for space TC links. Through a comprehensive
analysis and assessment of receiver functionalities for the TC uplink, we were able to identify the receiver bottlenecks and to propose
alternative receiver enhancements. The main outcomes and design
guidelines resulting from the study are summarized in Table 6.
The study provides an explicit demonstration of the feasibility
of the new receivers, paving the way for a more effective management of TC links in future missions.
ACKNOWLEDGMENT
The present contribution describes the achievements obtained
within the ESA's Basic Technology Research Programme entitled
Next Generation Uplink Coding Techniques (NEXCODE), Contract No. 4000111690/14/NL/FE, led by Deimos Engenharia, Portugal, as prime contractor.
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IEEE A&E SYSTEMS MAGAZINE
JUNE 2017
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