The invention discloses a flight parameter
signal generating
system. The
system includes an upper computer man-
machine interaction interface and a lower computer
signal generating
system, wherein thelower computer
signal generating system includes an engine system module, a
hydraulic pressure fuel oil system module, a power system module, a navigation attitude system module, a
bus system module and the like. LabVIEW is adopted for designing the upper computer man-
machine interaction interface, an Access
database is selected for storing parameter
data set by an upper computer and a lower computer communication network is constructed by taking an STM32 as a main control module in combination with RS485 technology. Switching quantity signals are achieved by adopting a single-
chip microprocessor in combination with a photovoltaic coupler. Analog quantity signals are generated through controlling a DAC
chip by the single-
chip microprocessor. AC rate signals are generated through an AC ratetable. Generation of
synchronizer signals is realized through a chip AD9959. Generation of ARINC429 is realized through controlling HS-3182 and HS-3282 by the single-chip
microprocessor. Generation of
AC power signals is realized through a
voltage transformer. A DC power supply power source is achieved through a
voltage stabilizing chip. Flight parameters are allocated to different signal generation modules. On one hand, management is facilitated. On the other hand,
design margin is realized and addition and reduction of signal generation modules are facilitated.