The invention discloses a ground-space-based integral measurement and
control system applied to a terrestrial space. The
system includes a ground measurement and control
station; a
relay satellite; anair vehicle including an upper antenna, a lower antenna, a
radio frequency front end, a transceiving
assembly and an air vehicle management computer, wherein the upper antenna and the lower antenna are used for receiving and transmitting of ground-base uplink and downlink signals and space-based forward and backward
remote control signals; the
radio frequency front end is used for performing filtering
hybrid amplification on signals and outputting the signals; the transceiving
assembly is used for conversion through modulation and
demodulation and for receiving CCSDS remote measurement framesor acquiring positioning information according to remote measurement parameters of the transceiving
assembly itself and calculating the optimal direction transmission of the space-based forward
remote control signals; the air vehicle management computer is used for transmitting the received positioning information and the calculated optimal direction of the space-based forward
remote control signals to the
radio frequency front end for
transmission switching between the upper antenna and the lower antenna and transmitting selected space-based backward remote control signals to the
relay satellite. According to the invention, a ground-based and a space-based remote measurement and remote control links can be implemented at the same time and whole course coverage of flight tasks is realized.