I am programming my own A320 homecockpit with C++.
At the moment I am at the descent and TOD calculation. In the manuals of Airbus, I couldn't find any fitting formula and I don't want to enter any rule of thumb.
I've read that some developers use the airfile to calculate the descent path. Does anybody know how that is done or maybe a way I could do it?
My workaround could be to do testflights with high weight and low weight, with fast IAS and slow IAS and interpolate between all those numbers. But I would prefer a more precise way.
Thank you
Julius
At the moment I am at the descent and TOD calculation. In the manuals of Airbus, I couldn't find any fitting formula and I don't want to enter any rule of thumb.
I've read that some developers use the airfile to calculate the descent path. Does anybody know how that is done or maybe a way I could do it?
My workaround could be to do testflights with high weight and low weight, with fast IAS and slow IAS and interpolate between all those numbers. But I would prefer a more precise way.
Thank you
Julius




