Automated design and implementation of satellite vibration test conditions

In response to the problems of long-time consumption and poor reliability in the formulation of satellite vibration test conditions, a general method for the concave design of vibration test conditions has been solidified, and an automated implementation tool has been developed. Firstly, based on the experience of formulating satellite vibration test conditions, a general method for concave design under vibration test conditions was constructed. Then, based on the concave design method under vibration test conditions, a concave design tool for vibration test conditions was designed from the perspectives of operational convenience and visualization; Finally, the concave design tool under vibration test conditions was applied to the formulation of satellite vibration test conditions, further verifying the application effect.