Double corrector for asymmetrical mechanism compensation
AssigneeSafran Aircraft Engines
InventorsChristophe Marc Alexandre Le Brun, Sébastien Jean Fernand Deneuve
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AssigneeSafran Aircraft Engines
InventorsChristophe Marc Alexandre Le Brun, Sébastien Jean Fernand Deneuve
Estimating the term…
The invention concerns a method for controlling a mechanism (10) displaying asymmetrical behaviour, the mechanism (10) comprising a first operating direction (F+) and a second operating direction (F−), the control method making it possible to generate, using a control module (24) of a computer (20), a control signal (x_com) from a setpoint signal (x_cons), in which—when the setpoint signal (x_cons) indicates that the mechanism (10) should be operated in the first direction (F+), the control module (24) applies a first corrector (100) to the setpoint signal (x_cons) in order to generate a control signal (x_com),—when the setpoint signal (x_cons) indicates that the mechanism (10) should be operated in the second direction (F−), the control module (24) applies a second corrector (100) to the setpoint signal (x_cons) in order to generate a control signal (x_com), and in which the first and second correctors (100, 200) have different parameters (Kp1, Kp2, Ti1, Ti2), in order to compensate for the asymmetrical behaviour of the mechanism (10).
A method for controlling a mechanism having a dissymmetric behavior, the method comprising the following steps:
A system,
A mechanism,
Dependencies are inferred from the claim text.