Stipe Gojanovic

Thank you for the fast response! I've managed to get it to work. Do you know why the values for variation in vertical speed, pitch and pitch rate start at such high values and if it is possible to determine realistic ones?

Hello all, I have been trying to do a stability analysis for a flying wing based on a 1/7 model of the YB-49 bomber for my university thesis, during the analysis I've encountered errors in the form of "Unsuccessful attempt to compute eigenvalues for Control". Any help with determining why that is would be much appreciated! I have attached the file.