Single and double pulse test system and method of high-power driving module for carrier rocket

The invention provides a single and double pulse test system and method for a high-power driving module for a carrier rocket. The test system can be suitable for design verification and batch test tasks of a rocket-borne high-power driving circuit. The system is integrated in a set of cabinet type testing device, required testing conditions are input through a man-machine interaction interface of control software, and after the lower computer controller unit integrates information of the upper computer and confirms that all the testing conditions are available, the testing work is automatically completed. After the test is completed, the upper computer automatically reads the voltage and current information captured by the oscilloscope, carries out data analysis and processing, and generates an experiment report. According to the invention, according to aerospace model test requirements, under any test conditions within a system function range, new research product function preliminary ...