Minimization of tumbling strength due to the Coriolis force of the centrifugal force-based flight simulator

摘要

According to the trainee in centrifugal force-based simulators, systems and methods for minimizing or removing a plurality of tumbling sensation caused by the Coriolis force is described. In one exemplary methodology, the simulator in order to reproduce a plurality of flight conditions in which a plurality of G force is reduced relative to the trainee to nominal G force value from the first G force value, the rotation of its shifting the speed. Before reaching the nominal G force value, is greater than the nominal G force value smaller middle G force value than the first G force value, between the appropriate duration, provided to a trainee, it is maintained. The intermediate G Chikarachi may be determined based on several factors including the angle of rotation of the gondola, and / or (ii) a first G force value, between (i) the first G force value. Intermediate G force value is applied between the appropriate duration, after being maintained, a plurality of G force applied to a trainee may be further reduced until it reaches the nominal G force value.