The invention provides a
system for testing a wired measurement and control interface of a
deep space exploration surrounding device to a lander. The
system comprises a main control module, an OC gate instruction receiving module, a
voltage remote measurement
simulation module, a
thermistor simulation module, an RS422 communication
simulation module, a heater simulation module and a power supply module. The OC gate instruction receiving module, the
voltage remote measurement simulation module, the
thermistor simulation module, the RS422 communication simulation module and the heater simulation module are all connected to the main control module; and the OC gate instruction receiving module, the
voltage remote measurement simulation module, the
thermistor simulation module, the RS422 communication simulation module and the heater simulation module are all connected to the power supply module. According to the invention, the function of the surround device to the lander wired measurement and control interface can be tested before the surround device is in
butt joint with the lander electrical interface, the
correctness of the interface and the coordination of information interaction are fully verified, and abnormal communication or potential safety hazards between the two devices caused by mismatching of the interfaces after the two devices are in
butt joint are avoided.