I'm not a fluids engineer so I invite help with specifics. I see some common control responses among various machines. While heavy equipment blades and buckets are controlled using internal hydraulic pumps, airplanes are controlled using external airflow changers. Where dynamic proactive control movement is necessary to nail a target, pump capability or airspeed determines whether fine or gross control movement is more effective.
The slowness of blade movement made control of the old cable controlled equipment awkwardly gross. Early pumps were weak resulting in similar gross control. Modern hydraulic pumps allow fine dynamic proactive precision. If old, don't use hand tools even for little dirt digging jobs. Rent a baby trackhoe and learn dynamic proactive control movement in ten minutes.
Airplane control movement is just as easy to learn. Fineness or grossness of control movement necessary is determined by the speed of relative wind over the particular control surface. I say particular because only the rudder and elevator receive prop blast. Dynamic proactive bracketing is possible with rudder or elevator but not with aileron.
Something I like to indoctrinate early is that the amount of rudder or elevator control movement is not critical so long as it is dynamlc and proactive. So to taxi the tailwheel airplane I require rapid and gross left right left dynamic proactive rudder movement to the stop to keep the yellow taxi line between our legs. This teaches where the rudder stop is, the necessity of keeping the target between our legs, the necessity of slow taxi, and the effectiveness of gross dynamic proactive control movement when slow. Dynamic proactive rudder movement needs to change from gross to fine as we accelerate on takeoff and change from fine to gross as we roll out on landing. Gross dynamic proactive elevator control helps bracket level fuselage in low ground effect just after we use aft elevator to get into low ground effect. Finer dynamic proactive elevator movement works as we accelerate in low ground effect.
Everyone learns that gross control movement is necessary when slow and finer control movement is necessary as we speed up, but an effective teaching point is that the grossness or fineness is not critical so long as it is dynamic and proactive. If we bracket the centerline between our legs continuously and faithfully, we are good. We need not worry about recovery from the start of ground loop if we simply bracket the centerline between our legs. No ground loop can happen so long as we keep walking the rudder dynamically and proactively to bracket the target. We don't have to sweat the timing for torque, gyroscopic precession, and P factor. We don't have to jab back if we don't allow lurch. We are already making quick and minor jabs continuously to bracket the centerline to prevent the lurch. Like Sundance in Butch Cassidy and the Sundance Kid, we're better when we move.
So just as quick blade control reaction to a stuck blade killing the engine on a dozer is not effective, quick rudder or brake reaction to longitudinal misalignment on the ground is not effective. Nor does quick aileron reaction to a turn on final maintain the centerline extended. Only using the anti-turn control, the rudder, dynamically and proactively to bracket the centerline will maintain the centerline extended. Will reaction work? Yes, if in time on the ground. No, never on final. Will making small correction turns on final ever bracket the centerline? No. Will not continuously walking the rudder on the ground eventually bite? Yes! Can fine dynamic proactive rudder work with nosegear airplanes? Absolutely!
Reaction to the start of ground loop is too late to be fine. It is late and has to be gross to be effective. It initiates gross dynamic reactive rudder movement to return to a bracketed equilibrium. Dynamic proactive braking is upset recovery.