The invention discloses an S-band unified carrier measurement and control device applied to a
spacecraft return
tail section, which receives a
spacecraft S-band
signal through a small omnidirectional /
directional antenna and transmits the
spacecraft S-band
signal to a high-frequency receiving subsystem; the high-frequency receiving subsystem amplifies and converts the
signal and inputs the signal into a
baseband to realize telemetering
demodulation and voice transmission; the transmitting subsystem processes the
baseband signal and amplifies and feeds the
baseband signal to the spacecraft. Meanwhile, a
data analysis module is designed to generate the flight path of the observation
station system according to the
data analysis data of the control center. The data forwarding control module adopts a multi-thread framework, analyzes telemetering data through a PDXP format, and forwards and executes point selection
processing based on a dynamic
routing table; the preferential
algorithm preferentially selects telemetering data with normal synchronous codes for forwarding, and the priority is determined by the real-
time distance between the equipment and the spacecraft. According to the design, the problems that traditional equipment is large in size, low-elevation-angle signals are weak and depend on
data transmission forwarding are solved, light weight, close deployment and
independent data transmission are achieved, and the measurement and control reliability of a spacecraft returning
tail section is remarkably improved.