Common control system and method for spacecraft load experiment process

The invention provides a common control system and method for a spacecraft load experiment process. The method comprises the following steps: step 101), information related to the operation of the load experiment process is defined and initialized; step 102), a set of all the actions of various space load devices is defined, and the set of all the actions comprises all the actions that need to be executed by various loads to achieve the functions of the various loads; step 103), with each experiment batch serving as a unit, the execution time and action number of each action of each batch of experiments are listed, and the specific execution details of each action are determined according to the action set defined by a load list; step 104), the actions or the current statuses of all the loads are monitored, a discovered abnormality in the status of each monitored load is handled according to a saved strategy, and the strategy is a set of a plurality of actions.