I am trying to improve a plane by adding a forward fin to it and changing its engine. But this will obviously move the c.g., so it's derivatives will also change. Any suggestions how this is achieved is still welcome.
Thank you for your reply.
Well, I have the stability and control derivatives for my aircraft, all calculated with respect to the c.g. assumed at the origin of the body axes (nominal c.g.). Now I found out that the final c.g. is displaced in the Ox and Oz directions by some distances. I believe...
Hello,
I am trying to develop a MatLab program that mathematically models an aircraft in trim flight. Everything fine so far, except that the reference system used does not coincide with the centre of gravity. I denoted the distances from the origin of the reference system to the centre of...
