Common control system and method for spacecraft load experiment process

Abstract

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.

Description

technical field [0001] The invention relates to the technical fields of aviation and aerospace electronics integration, generalization, and modularization, and more specifically relates to a general control protocol for a spacecraft load experiment process, and provides a spacecraft load experiment process control system and method. Background technique [0002] The payload equipment for scientific experiments on spacecraft has the following characteristics: various types, unique functions, high reliability and safety requirements, complex control process, scientific requirements, and uncertain and changeable experimental parameters. Usually, the load control management software or FPGA is only specially developed for the specified load equipment. This development mode has a long development cycle, poor versatility, and reliability cannot be guaranteed, which increases the development cycle and development cost of the load equipment; at the same time, because there is no inh...

AI Technical Summary

Problems solved by technology

This development mode has a long development period, poor versatility, and reliability cannot be guaranteed, which increases the development period and cost of the load equipment; at the same time, because there is no inheritance, each equipment is completely re-developed, so the safety and reliability of the system are increased. sexual risk

Today, with the rapid development of aerospace technology, this development model can no longer meet the requirements of the development of payload equipment

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