The invention provides an anti-
noise high-precision error vector amplitude measurement
system and method for a
satellite launching
system. The
system comprises a demodulator, an A / D conversion circuit, a data
distributor, a decoding function module and an EVM
processing module. And the demodulator carries out
carrier synchronization, code synchronization and
blind equalization processing on the
digital signal, and outputs real I-path data Ireal and Q-path data Qreal. The data
distributor copies the Ireal and the Qreal and divides the Ireal and the Qreal into two paths for output, one path is transmitted to the decoding function module, and the other path is transmitted to the EVM
processing module. And the EVM processing module comprises a
phase error calculation unit, an amplitude error calculation unit and an error vector amplitude calculation unit which are respectively used for carrying out
parallel processing on the Ireal and the Qreal, calculating to obtain a
phase error ErrPhase, an amplitude error ErrMag and an error vector amplitude value, and reporting an analysis and processing result through a CPCI (Compact
Peripheral Component Interconnect)
bus. According to the invention, high-precision and anti-
noise measurement of the
satellite emission
signal quality is realized through shunt
parallel processing and a multi-bit-width quantization and
smoothing strategy.