Research on three axis air bearing platform simulation system for small satellite attitude control

In this paper, a simulation system of three axis air bearing platform for micro satellite attitude control is designed. The technical features of the experimental system are also given. The simulation system is introduced in detail from the aspects of the overall design, actuator, attitude measurement system, control system and gravity center adjustment system. The experimental ability of the simulation system is verified by a series of experiments. The simulation system can lay a good foundation for the subsequent research on agile attitude control of micro satellite.