I believe that all Gyrocopters pilots know that they need to take off with a minimum rotor rpm before apply full power. Is the very first thing that Instructors teach in takeoff.
In this chat you are calling the rotor instability because of too low rotor rpm blade sailing and retreating blade stall. However, it is not blade sailing and it is not retreating blade stall.
Blade sailing is the uncontrolled blade flapping caused by wind. It is of big concern when slowing down rotors in windy conditions, because the blade can hit the tail boom. Of course, this will be the result of trying to take off with too low rotor rpm, but the cause is not “blade sailing”.
Retreating blade stall happens because too fast IAS. It implies that the retreating blade has to work in a too high angle of attack and it stalls… The effect in the aircraft is a nose up or down depending on the rotor spinning side. However, what happens when trying to take off with too low rpm is a very bad and rough lateral flapping and a turn over.
The real reason of this undesirable phenomena is the lack of enough centrifugal force on the blades. A rotor, to be stable, needs the rigidity provided by centrifugal force, that is about 2500 kg (more than the doble in pounds) for an ELA rotor spinning at 360 rpm. Each blade is supporting about 230 kg of lift, and the ratio with centrifugal force give a small rotor conning angle and restrain the flapping movement.
The problem in takeoff is that we don´t have a direct control of rotor rpm. The easy solution is to prerotate the rotor to a safe level regime. In spite of rotor rpm decay in the first seconds of takeoff roll the centrifugal force will be big enough to provide rotor stability during all takeoff and continuous flight.
The problem arises when we request lift (by pulling the stick aft combinate with too great the air speed). The air speed can be provided by the pilot because of selected power or by the wind if it is strong enough. Then the ratio between lift/centrifugal force is too high. The advancing blade tries to climb to equalize lift in the two sides of the rotor. The retreating blade does the some by going down. But because of the lack of centrifugal force the flapping is too big, the rotor hits the stops and the bad flapping occurs. The rotor is unable to compensate de dissymmetry of lift and the gyrocopter turns over.
It is possible to take off safely from very low rotor rpm (60 rpm). In negligible wind condition we pull the stick full back and the without delay we apply little power, just to produce forward very slow movement (the speed of a walking man). The we wait until we can see that rotor rpm are increasing. Immediately you will feel that the forward speed is slowing down. Keep the speed by increasing power. Now two options, when you get the safe rotor rpm (210 rpm in the ELA) apply full power and perform a normal takeoff. Or continue maintaining low forward speed until the nose goes up: then full power.