calculate two drone setups given thrusts and position of each of the rotors

Aerospace/aeronautical engineer needed to calculate two drone setups (2 versions of positioning) given thrusts and position of each of the rotors; simulate the movement and the flight attitude on a straight track and on a curved path (at least 15 curves of different degrees; 5 of the curves in a "zig-zag" path on a straight point-a to point-b destination). The output should be the simulation results, the attitude expectations at 3 different speeds (40%, 75% and 100% of full thrust), possibly the simulation videos and an estimation of the most efficient setup on both the tracks (straight and curve). As expected output, would be great a maneuverability report and expected radius for 90 degrees turning. The two versions are: - A: It's a quadrotor but the two rear rotors are not aligned with the front ones. - B: It's a quadrotor but the two rear rotors are not aligned with the front ones, but centered on the middle axis; the two rotors are one on the top of the other, but one facing up and one facing down. So the scheme is an "Y" but it is a quadrotor. Each motor will have a full maximum thrust of 180kg . (total mass carried in average 250kg) Please find attached the schemes of the versions A and B in an aerial view. The simulation program can be choosen by you and what you consider more appropriate/efficient: virtual studio or ansys or whatever. Here find in the second part of the of these links (the gifs/videos) something like what I would like to see (the separated and compared tracks of the setups) on the different movement simulations described before: [login to view URL] [login to view URL] also note that the "head" of the drone is looking left on the images and please remember to add videos/gifs of all the scenarios along with the data resulting; If possible a gif comparing both setups together and eventually a track of the path followed