The invention provides an FPGA (
Field Programmable Gate Array) based ground launching control device of a small and medium-sized
rocket. The device comprises a main control computer, a ground control box, a
signal conditioning case which uses FPGA as the core, and a
missile device; the main control computer receives and feeds back a
signal through an RS422
communication interface; the ground control box is used for performing hardware control for the
system; the
signal conditioning control case comprises the combination of a PCB and a power supply; the PCB comprises a level isolation conversion circuit which uses the FPGA as the core, a power-on
sequence control circuit, a
voltage AD acquiring circuit, an RS422 isolation conversion circuit, an RS422
relay circuit, a level conversion circuit in a head power supply circuit, and a corresponding filter circuit; the
missile device comprises a
missile distributor, a missile battery combination and a missile electrical device. With the adoption of the device, the functions of supplying power to the missile device from the ground, activating the missile battery, converting power,
cutting off power supply, controlling a
pressure release valve, and controlling ignition can be realized; the device has the characteristics of being safe, reliable, small in cost, short in development cycle, fast in speed, high in efficiency, and high in real-time performance.