Reliability and effectiveness are essential features of satellite transceivers for telemetry and telecommand applications. Modem performance has a strong impact on the success of a satellite mission, in particular, during critical scenarios as the early operation phase, the disposal of a satellite at the end of its life, or the deep-space missions. In these specific mission critical scenarios, fast and correct data reception is even more important than high channel capacity. An unknown and fast variable channel condition, which can be caused by uncertain spacecraft attitude and large Doppler shift with respect to the data rate, requires efficient and innovative receiver architecture. This paper introduces a complete digital implementation of a transceiver for TM/TC application in low Earth orbit mission that is perfectly compliant with aforementioned requirements. Particular attention is dedicated to the definition and selection of the most appropriate frequency recovery technique; 2 open-loop techniques that are derived from ML optimal estimator are presented and compared. Additionally, the performance of the proposed receiver is extensively studied and compared with an incoherent technique that is based on the double differential PSK modulation and is known to be suitable for sat-com in critical scenarios.
KEYWORDScritical scenarios, frequency recovery, satellite modems, telemetry and telecommand applications
INTRODUCTIONThe success of a space mission strongly depends on the quality and performance of satellite subsystems. The Telemetry and Telecommand (TM/TC) is an essential module for a spacecraft along with the electrical power system, on-board data handling and attitude and determination control system.The availability of the communication link with the satellite from the early mission phase allows the ground operator to monitor satellite status and to perform recovery actions if something goes wrong; an on-board computer failure may be recovered by rebooting the associated power line through a direct telecommand to the electrical power system.The early operations after separation from upper launcher stages, as well as the end of life disposal manoeuvres, are critical satellite mission phases that require a robust and reliable communication system. 1,2 In these scenarios, the spacecraft may have reduced functionalities and uncontrolled attitude, and consequently, the communication link could be weak and unstable, eg, signal's amplitude may be subjected to deep fading according to satellite tumbling rate. 3 In this context, the communication becomes bursty and the link reliability harms the bit-rate performance.Moreover, new challenges are receiving the interest of the space communication community. Nowadays, an innovative and popular way to access space is by means of new low-cost satellite solutions such as micro or nano-satellites. 4,5 These systems have typically less stringent performance requirements when compared with traditional space systems but, on the other hand, limited energetic and computationa...