The time scaling is 1:10

During this operation, the rotors have a low forward winding speed of about 7.0 m/s, consuming a power of 13.0 kW. The aircraft is decelerating horizontally at a rate of about 0.041g, having a horizontal speed of 29.59 m/s. At the same time, the aircraft has a vertical descending speed of 5.67 m/s, which is decreasing at a rate of 0.01g. Inflow stays 2.64 m/s. The aircraft operates like a lift going up at a speed of 1.52 m/s under a gliding wing with the equivalent LDR of 3.5. The aircraft is handled by using the __biangular handling__ based on angles of attack with values of 30.0° and 8.0°. The rotors have a __PGS-state__ (18.3°, -6.4°, -5°) with the increased pitch, the reversed gain and the decreased inclination of the skew.

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