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Method and a device for providing assistance in piloting a rotorcraft at takeoff
Method and a device for providing assistance in piloting a rotorcraft at takeoff
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机译:在起飞时为旋翼航空器提供协助的方法和装置
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摘要
The invention relates to a method of piloting a rotorcraft having a plurality of engines for driving at least one lift and propulsion rotor, in which method, so long as the rotorcraft has not reached an optimum climb speed (OCS), a pitch attitude control signal (Upitch) is determined that is adapted so that the rotorcraft accelerates in application of a profile (P1, P2, P3) that varies as a function of the elapsed time and as a function of the operating state of the engines (OEI/AEO).
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