I would put it this way;- If your collective pitch pull is aggressive then it will induce corolois effect, if it is not aggressive then the centrifugal force of the blades mass (as a force in balance against the aircraft weight) will resist upward coning.
Have a look at a fixed wing aircraft;- pull the stick back slowly the aircraft attitude changes and the aircraft climbs gracefully without any perceived wing bending. Pull it back violently and the blessed wings come off upwards. (the strength of the wing structure resists bending up to the engineered design limit)
In reality you should only need to think about Corolois effect as a very useful tool to make it work for you in unpowered flight. (a lot less centrifugal force makes it easier to use)
The drag AC talks about happens after the corolois bending.
Getting a correlator (throttle or cam box) to work well is an art and on some models after a few hours wear you might wonder why they are even there.