Dropping the speed and the descent rate at altitude 2m

 

Liftoplane: dropping the speed and the descent rate at altitude 2m RSI: dropping the speed and the descent rate at altitude 2m

The time scaling is 1:10

  During this operation, the rotors have an increased moderate forward winding speed of about 16.6 m/s, consuming a power of 35.3 kW. The aircraft is decelerating horizontally at a rate about of 0.225g, having a horizontal speed of 25.98 m/s. At the same time, the aircraft has a vertical descending speed of 2.24 m/s, which is decreasing at a rate of 0.145g. Inflow increased to 3.27 m/s. The aircraft operates like a lift going up at a speed of 4.82 m/s under a gliding wing with the equivalent LDR of 2.0. The aircraft left the "stream following" mode of operation, having a horizontal position of the fuselage, and it is handled by using the biangular handling based on pitches with values of -4.2° and 42.4°. The rotors have a PGS-state (17.0°, -39.3°, -5°) with the additionally increased magnitude of the negative gain.

 

 

Dropping the speed and the descent rate at altitude 6m Before touchdown at altitude 0.4m

 

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