| 摘要 |
The invention relates to a method of automatically managing the flight of an aircraft in turbulent air comprising notably the determination of the current speed (V<SUB>c</SUB>), of an optimal turbulence speed (V<SUB>t</SUB>), of a current thrust value (P). The data relating to a turbulence is acquired. An optimal turbulence speed is determined. Measuring a deviation (Delta) between the current speed (V<SUB>c</SUB>) and the turbulence speed (V<SUB>t</SUB>). Comparing the deviation (Delta) and a maximum deviation value (Delta<SUB>max</SUB>). Iterating k times of the previous three steps, to determine whether the deviation (Delta) is greater than the maximum deviation (Delta<SUB>max</SUB>) for the k<SUP>th </SUP>consecutive time, and the readjustment of the current thrust (P) so as to reduce the deviation (Delta) to a value less than that of the maximum deviation (Delta<SUB>max</SUB>) and to make the current speed (V<SUB>c</SUB>) converge to the turbulence speed (V<SUB>t</SUB>).
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