| 摘要 |
The present invention relates to a rotorcraft (1) extending in a longitudinal direction along a first forward-backward plane (P1) separating a first side (6) from a second side (7) of a rotorcraft (1). The rotorcraft (1) comprises: at least one main rotor (5), an auxiliary rotor (10), and at least one airfoil (25). The rotorcraft (1) includes a processor unit (30) connected to a mover means (35) to pivot the airfoil (25). The processor unit (30) is connected to a first measuring system (41) to measure a present value of a speed parameter (V) of the aircraft (1), and is connected to a second measuring system (42) to measure a present value of a power parameter (W) of the power plant (90) to control a deflection angle of the airfoil. |
