CamJPete
Structural
- Jan 30, 2019
- 25
Suppose you have an assembly that will go on a launch vehicle and be subjected to random vibration. Also suppose the input random vibration PSD (acceleraton spectral density) is given in the launch vehicle coordinate system, with the X-axis aligning with the axial direction, and Y-axis aligning with lateral.
If the payload is mounted at some angle, suppose 10 degrees off from axial, how would you derive a new input to be inline with this new rotated coordinate system? If it were a static vector in axial and lateral, you could simply take the components of each vector in the new axis. But since the loads vary with time and vary over the frequency range, I don't think it's as simple as taking the components.
I'm wondering if I need to synthesize a time history in the axial and lateral directions from the respective PSD's, then combine the time histories in the new axis that accounts for phase differences, then calculate the PSD from the combined time history.
Thoughts on this? Thanks.
If the payload is mounted at some angle, suppose 10 degrees off from axial, how would you derive a new input to be inline with this new rotated coordinate system? If it were a static vector in axial and lateral, you could simply take the components of each vector in the new axis. But since the loads vary with time and vary over the frequency range, I don't think it's as simple as taking the components.
I'm wondering if I need to synthesize a time history in the axial and lateral directions from the respective PSD's, then combine the time histories in the new axis that accounts for phase differences, then calculate the PSD from the combined time history.
Thoughts on this? Thanks.