State-of-the-art space mission telecommand receivers
Marco Baldi, Massimo Bertinelli, Franco Chiaraluce, Pau Closas, Pawan Dhakal, Roberto Garello, Nicola Maturo, Mònica Navarro, José M. Palomo, Enrico Paolini, Stephan Pfletschinger, Pedro Freire da Silva, Lorenzo Simone, Jordi Vilà‐Valls · IEEE Aerospace and Electronic Systems Magazine · 2017
Since their dawning, space communications have been among the strongest driving applications for the development of error correcting codes. Indeed, space-to-Earth telemetry (TM) links have extensively exploited advanced coding schemes, from convolutional codes to Reed-Solomon codes (also in concatenated form) and, more recently, from turbo codes to low-density parity-check (LDPC) codes. The efficiency of these schemes has been extensively proved in several papers and reports. The situation is a bit different for Earth-to-space telecommand (TC) links. Space TCs must reliably convey control information as well as software patches from Earth control centers to scientific payload instruments and engineering equipment onboard (O/B) spacecraft. The success of a mission may be compromised because of an error corrupting a TC message: a detected error causing no execution or, even worse, an undetected error causing a wrong execution. This imposes strict constraints on the maximum acceptable detected and undetected error rates.