I flew a flight test of the Balerit for a flying mag years ago. It was the nearest thing to a foolproof aircraft (if there is such a thing) that I ever met. Stick back in your gut, boot in the pedal (no ailerons) and it just went round the turn nodding gently but impossible to stall, and I tried! Anybody trained on it would have been lethal on anything else. It's only problem was crosswind landings. Couldn't yaw it straight as it immediately rolled away from the wind. Couldn't use wing down technique as no ailerons, so just had to put it down and let the undercarriage take the strain, which to be fair, it did. It was just a microlight with tandem wings and therefore lots of drag with all the struts etc.
Both characteristics are shared with some other non-Mignet designs. Sequential stalling and unstalling of the front wing is also how more recent canard aircraft work, e.g. Rutan designs and similar.
Ercoupes have the same characteristic in a crosswind landing as a result of having interconnected ailerons/rudder and no pedals other than one for the brakes. In that circumstance the Ercoupe is designed to be flown on in a nose high crab, something quite easy to do, with the main gear built heavily to take the side loads. A while ago I was surprised to read a test on the Ercoupe which didn't understand this procedure and said crosswinds were a problem in the type! The trick is let the tricycle gear do its thing and crab it on with controls neutral. The plane will yaw itself into line after the main gear touches down. If the pilot instead attempts to straighten the yaw himself, the nose wheel may be turned when it touches, possibly resulting in a wheelbarrow-style ground loop. Also as noted the wrong wing is raised. I imagine the same technique might work on a rudder + dihedral controlled Mignet plane, assuming it has tricycle gear and assuming its built for the job.