Wind generating set operation parameter control method and system, equipment and storage medium
A technology for wind turbines and operating parameters, which is used in the control of wind turbines, mechanical equipment, and engine control. Effects of Functional Stationarity Problems
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Embodiment 1
[0044]A method for controlling operating parameters of a wind turbine based on spline interpolation, comprising the following steps:
[0045] Step 1) Set the control cycle, obtain the pitch angle data in the control cycle, and obtain the pitch angles of the two endpoints in the control cycle, which are respectively the initial pitch angle and the termination pitch angle;
[0046] Step 2) obtain current pitch angle;
[0047] If the current pitch angle is less than the initial pitch angle, then use the proportional gain parameter setting value corresponding to the initial pitch angle to calculate the pitch angle command;
[0048] If the current pitch angle is greater than the end pitch angle, the pitch angle command is calculated using the proportional gain parameter setting value corresponding to the end pitch angle.
Embodiment 2
[0050] A method for controlling operating parameters of a wind turbine based on spline interpolation, comprising the following steps:
[0051] Step 1) Set the control cycle, obtain the pitch angle data in the control cycle, and obtain the pitch angles of the two endpoints in the control cycle, which are respectively the initial pitch angle and the termination pitch angle;
[0052] Step 2) obtain current pitch angle;
[0053] If the current pitch angle is less than the initial pitch angle, the pitch angle command is calculated using the integral time constant corresponding to the initial pitch angle;
[0054] If the current pitch angle is greater than the end pitch angle, the pitch angle command is calculated using the integral time constant corresponding to the end pitch angle.
Embodiment 3
[0056] A method for controlling operating parameters of a wind turbine based on spline interpolation, comprising the following steps:
[0057] Step 1) Set the control cycle, obtain the pitch angle data in the control cycle, and obtain the pitch angles of the two endpoints in the control cycle, which are respectively the initial pitch angle and the termination pitch angle;
[0058] Step 2) obtain current pitch angle;
[0059] If the current pitch angle is smaller than the initial pitch angle, the differential coefficient corresponding to the initial pitch angle is used to calculate the pitch angle command;
[0060] If the current pitch angle is greater than the end pitch angle, the differential coefficient corresponding to the end pitch angle is used to calculate the pitch angle command.
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