一种四自由度卫星模拟装置
By designing a four-degree-of-freedom satellite simulation device, and using air buoyancy combined with reverse counterweight and symmetrical pulley system, the satellite was able to translate along the X, Y, and Z axes and rotate around the Z axis on the ground. This solved the problems of low accuracy and high maintenance cost in existing microgravity simulation technologies, and provided high-precision attitude control.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- BEIJING RES INST OF PRECISE MECHATRONICS CONTROLS
- Filing Date
- 2023-04-17
- Publication Date
- 2026-07-17
AI Technical Summary
Existing satellite microgravity simulation devices are unable to achieve equivalent simulation in all dimensions, especially in terms of attitude control of the four degrees of freedom: translational motion along the X, Y, and Z axes and rotation around the Z axis. They also suffer from problems such as high friction, high maintenance costs, and low accuracy.
Design a four-degree-of-freedom satellite simulation device. Based on the air flotation method, combined with reverse counterweight and symmetrically distributed pulley system, the device achieves four-degree-of-freedom motion by controlling the gas supply time and pressure of the air supply and nozzle through the pressure system, including translation along the X-axis, Y-axis and Z-axis and rotation around the Z-axis.
It achieves high-precision microgravity simulation of satellites on the ground, reduces the impact of friction, lowers maintenance costs, and improves the simplicity and accuracy of attitude control.
Smart Images
Figure CN116495206B_ABST