That is doable. A variable pitch propeller is necessary to achieve it.
Looks like I missed something here, but since question was answered in 3rd comment and I am not going to mess with C++ problems and sphere geometry, I will put only few comments.
So - As Paul mentioned, the light prop was developed especially for easier RPM controll. As Brett mentioned its (the prop) and motor mass inertia moment limits bandwidth, it is very imprtant for controll. That is also reason why I stick with small diameter motors (2826 - like AXI). We tested also MVVS which has stator diameter 35mm and difference was obviouse.
BUT there is also another problem, thrust controlled by RPM is asymetric, means prop can better pull than brake. Reasons are 2 - the first is chambered airfoil, that was another object of optimization for new props, and second is lower RPM during braking also means lower reaction to model speed changes (the same prop at higher RPM will change the thrust as function of speed difference more that the same prop at lower RPM).
That means that pitch controlled prop will not only react quicker (with quick servo - I do not think it will be so quick with normal servo - reaction time of classic servos is not much higher that reaction of my power train, I cen easily show that frequency of of RPM change input can be higher than standar R/C servo - we will use probably small light servo which can make run from one side to the other loaded at say 0.2s what is visible lag; but high speed servos working at 400Hz inputs will be probably enough).
However I am not sure if I want have such prop on contest model. Fixed prop is fixed prop and I am sure it will never dismuont during official flight, I can be sure that I can easily replace if we fly on typical WCh potato fields etc
But who knows, may be Mark will push it to reliable solution then I will think about it.