Correcting the closed orbit in PyAT

[elafmusa]

Hello everyone,

I am asking if there is a function for correcting the closed orbit in PyAT by calculating the strength of the required correctors?

I tried to implement that by constructing the response matrix but the results still not good.
I attach a file with my trial.

I'd appreciate your comment on the file
Correction.zip

[swhite2401]

Hello, I could only find a tex file, would you have a python script with your example?

[elafmusa]

Correction.zip

Hello, I attach the file again with the python script.
In my example i tried two methods to invert the response matrix: the pseudo-inverse which leaded to the orbit corrected to the value e-10 and i also tried the SVD method where i think something went wrong as the multiplication of the invers response matrix and the closed orbit gave more than 3 correctors strength values.

Thank you in advance