The time scaling is 1:10

During this operation, the rotors have an additionally decreased low backward winding speed of about 5.2 m/s, providing a power of 6.9 kW, which is used to recharge the accumulators. The aircraft is decelerating horizontally at a rate of about 0.051g, having a horizontal speed of 30.54 m/s. At the same time, the aircraft has a vertical descending speed of 5.10 m/s, which is increasing at a rate of 0.031g. Inflow increased to 2.62 m/s. The aircraft operates like a lift going down at a speed of 1.21 m/s under a gliding wing with the equivalent LDR of 5.5. The aircraft is handled by using the __biangular handling__ based on angles of attack with values of 23.0° and 6.0°. The rotors have a __PGS-state__ (13.1°, 34.3°, -10°) with the increased pitch and gain and the decreased inclination of the skew.

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