Satellite attitude track control test system and method

Abstract

The invention provides a satellite attitude track control test system and method. The satellite attitude track control test system comprises a simulator head, a simulator intelligent controller and a simulator remote client side, wherein the simulator head is used for outputting simulation signals in a test and simulating the operating environment of a satellite to be tested; the simulator intelligent controller is connected with the simulator head, controls the operation of the simulator head and collects the work state of the simulator head, and the simulator remote client side is connected with the simulator intelligent controller, controls the operation of the simulator intelligent controller remotely and displays the work state of the simulator head; the simulator remote client side is connected with the simulator intelligent controller through a bus. The satellite attitude track control test system and method can realize a simulator remote control function, carry out remote control and state display through the simulator remote client side, realize unattended operation of a test site, and improve work efficiency.

Description

technical field [0001] The invention relates to the field of aerospace testing equipment, in particular to a satellite attitude orbit control testing system and a system testing method. Background technique [0002] The satellite attitude and orbit control (attitude orbit control) test system is used for the ground test of the satellite attitude and orbit control subsystem. Some simulators (such as solar simulators) in the traditional satellite attitude and orbit control test system are not connected to the test network, requiring staff to manually operate the simulator at the test site, and remote automatic control cannot be implemented. [0003] Moreover, if some simulators fail to work, it may cause harm to the products on the star. For example, if the heating module of the earth simulator fails and the heating module continues to heat, if measures are not taken in time, it will cause damage to the infrared earth sensor on the star; If the rotation does not stop after r...

AI Technical Summary

Problems solved by technology

[0006] To sum up, the existing satellite attitude and orbit control test system relies on manual methods, which can no longer meet the requirements of remote automatic control of simulators, autonomous fault identification and processing of simulators, and automatic statistical processing of component test data.

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