Berkcan Kapusuzoglu
Berkcan Kapusuzoglu
Hi, thank you for the information. I have tried a two-stage rocket following your guideline. However, the second stage results copies the first stage results after the apogee. Basically, using...
I realized defining an initialsolution results in "'function' object is not subscriptable" error. Also, I tried single-stage rockets with an initialsolution (somewhere close to the aporgee) and realized that the...
I realized that the `initialsolution` should start from `tInit = 0.` Have you checked RocketPy for multi-stage rockets? Do you have any input data for it or can you suggest...
Also, I assume that we need to change the Euler parameters to the initial values when we are setting up the `initialsolution`. Otherwise, the rocket will not climb up in...
Thank you! What I did was very close to this. Only thing I didn't understand why Y and Vz are set to 0 for the second stage. When I set...
I think it is related to the fact that your test set is not providing the correct batch shape defined in `BatchIndependentMultitaskGPModel`.
what is the issue? Have you tried another model?