In my experience, during “g” or “accelerated” stalls, or autorotation induced with aileron lose or at the stall, the aircraft recovers very quickly with centralising controls. The real crucial factor is to unload or reduce AoA, that’s why ideally, get the stick forward of neutral. 2-3 turns of a spin will be considered fully developed when rates of roll, pitch, yaw are constant. In the incipient phase, roll, pitch, yaw are generally oscillatory, and the aircraft will also be transitioning from level flight, to a vertical spiral, around the spin axes. As I said, in the incipient phase, the moments of inertia in yaw, roll, pitch have not had time to build up. This is a generic consideration, some aircraft may well be fully into the spin earlier. But to me, there is a difference between the incipient and fully developed spin, and moments of inertia to me, will take more than 1 turn to fully develop.
at the end of the day, consider an autorotation, occurring in a base leg turn. Without spin training, power to idle, then centralising controls, making sure you unload enough to un-stall the wings, crucial. Most aircraft should recover. In a fully developed spin, most aircraft should recover, with controls held neutral, otherwise to me, they should not have been certified. The reason that positive spin recovery actions are taken, is recovery will be faster. Snapping on full opposite rudder may not be required, and my slight problem with this is, you need to remember to centralise the rudder immediately on recovery, or yaw roll to the opposite direction could occur, and possibly cause an autorotation to occur in the opposite direction. Again, look at the flight manual.