The time scaling is 1:10
During this operation, the rotors have a somewhat decreased moderate forward winding speed of about 16.5 m/s, consuming a power of 51.6 kW. The aircraft has a vertical acceleration of -0.034g and accelerates horizontally with a value of 0.071g by the gravitational force acting on the wings with the equivalent LDR of about 9.0. Inflow decreased to 2.18 m/s due to an increase in the horizontal speed of the aircraft to 38.33 m/s. The vertical speed remains at 1.67 m/s. The aircraft operates like a lift going up at a speed of 9.09 m/s under a fast gliding wing. The propulsion efficiency increased to 99.02 percent. The aircraft is handled by using the biangular handling based on angles of attack with values of 12.0° and 2.5°. The rotors have a PGS-state (1.9°, -38.6°, -5°) with the decreased pitch and the reduced magnitude of the negative gain.
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