Test and launch control system

Provided with a test and launch control system. The system comprises a vehicle-mounted test and launch control computer, a universal interface adapter, and a vehicle-mounted base module. The vehicle-mounted test and launch control computer is used for generating an instruction to realize rocket key time sequence control, programmable power supply control, information monitoring and remote launch control; an interface of the vehicle-mounted test and launch control computer is obtained by development based on LabWindows; the universal interface adapter is used for converting the instruction generated by the vehicle-mounted test and launch control computer into a switching value time sequence control signal required by a rocket system, CAN bus data required by a programmable power supply andRS422 bus data required by a remote control system; and the vehicle-mounted base module is used for realizing signal forwarding of communication between the vehicle-mounted test and launch control computer and a vehicle-mount