This invention proposes a multi-operating-point electric propulsion
beam control verification system, belonging to the field of
aerospace electric propulsion technology. It solves the problem that the electrical
coupling relationship between the shield,
anode, and accelerator cannot be simultaneously simulated under non-ignition conditions, forcing
beam control verification to rely on actual ignition. It includes an
anode current AD acquisition module, which acquires the
anode power
supply current value and transmits it to a processor for
processing via an internal communication module; an anode configurable load module, which configures the anode
load resistance value based on the anode resistance configuration result generated by the processor, thereby adjusting the anode
power supply voltage; a shield configurable load module, which configures the current of the shield load based on the shield current configuration result generated by the processor; an accelerator configurable load module, which configures the current of the acceleration load based on the acceleration current configuration result generated by the processor; and a storage module, which stores the anode power
supply current value and each configuration result.