Spacecraft system simulation collision damage adjudication system and method

Abstract

The application relates to a spacecraft system simulation collision damage judgment system and method based on a real-time judgment process, which comprises the following: a spacecraft system simulation business calculation module, which is used for calculation and output according to business demand and task targets, and realizes external data and clock transceiving through a spacecraft system simulation business calculation service; a plurality of damage judgment task modules; a simulation display module, which is used for interface design of input data and interface display of output data, and realizes external data transceiving and clock synchronization through a simulation display service; and a simulation scheduling support framework service module, which is interactively connected with the spacecraft system simulation business calculation module, the damage judgment task modules and the simulation display module, and is used for data receiving and distribution scheduling and clock synchronization control of the system. The application can form quantitative evaluation of target damage and objectively improve the evaluation result.

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