The invention discloses a
control system of a
solid-liquid dynamic
sounding rocket. The
control system is composed of a ground test launching control part and a
rocket-borne control part. The
control system is mainly used for realizing the following three tasks: converting ground power supply of a
rocket-borne device to
rocket-borne power supply, completing
test preparation before launching the
solid-liquid dynamic
sounding rocket to realize the functions of launching control, security control, and the like, and carrying out variable
thrust control on the
solid-liquid dynamic
sounding rocket and monitoring, collecting and recording the states. The invention provides a solid-liquid dynamic aircraft control
system. By utilizing the solid-liquid dynamic aircraft control
system, the functions of monitoring, ignition testing, emergency danger eliminating, and the like to the important rocket-borne device can be realized before the rocket is launched, the rocket-borne control part can realize thrust adjustment control according to control requirements after the rocket is started, and liquid
propellant main road and side road channel valves are controlled according to the control requirements to clear residual
propellant in a channel after the flight mission is finished. Meanwhile, real-
time data acquisition and recording on parameters for reflecting working conditions of a solid-liquid
rocket engine are carried out by the rocket-borne control part in the entire
flight process.