This invention relates to the field of
ground testing technology for
spacecraft attitude control systems, specifically providing a
ground testing method for the accuracy of a multi-level composite
attitude control system. First, a fully physical
simulation ground testing platform is constructed, including an on-
orbit environment
simulation system and a multi-level composite
attitude control simulation system. Two reference calibration devices are built using a calibrated dual-axis photoelectric
autocollimator, and two measurement reference units are constructed using the dual-axis photoelectric
autocollimator and a multifaceted
prism. Based on a cubic mirror, the calibrated dual-axis photoelectric
autocollimator, and the dual-axis photoelectric autocollimator, zero-position reference calibration and angle calibration are performed on the multi-level composite attitude control
simulation system. After calibration, the multi-level composite attitude control
simulation system is controlled to move from the initial position to the final position, and angle information is collected through the two measurement reference units. The attitude control accuracy is calculated based on the angle information. This invention realizes ground testing of a multi-level composite
attitude control system based on fully physical simulation.