Reference signal self-extraction active vibration control method for piezoelectric intelligent structure
A technology of reference signal and intelligent structure, applied in electrical components, adaptive network, impedance network and other directions, can solve the problem of difficult to obtain accurate reference signal and so on
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Embodiment 1
[0063] The reference signal self-extraction active control method of piezoelectric intelligent structure vibration, the specific operation steps are as follows:
[0064] (1) Carry out model identification on the control channel, and obtain the model identification parameters
[0065] ① Set the identification model filter order, step size factor, and identification error critical value, and select the excitation signal as the reference signal.
[0066] ②Set the excitation frequency and turn on the exciter to keep the piezoelectric smart structure in a state of continuous vibration;
[0067] ③ Use the minimum mean square error algorithm to adjust the model filter weights.
[0068] (2) Set the corresponding parameters and initial values of the control algorithm
[0069] Including setting the control structure filter order and step factor, while referring to the signal The initial value of is selected as a random noise signal.
[0070] (3) Synthesize the reference signal ...
Embodiment 2
[0079] This embodiment takes the active vibration control of the piezoelectric intelligent structure of the simulated aircraft frame as an example, and the description is as follows:
[0080] see figure 1 and figure 2 As shown, this reference signal self-extracted piezoelectric intelligent structure vibration active control method is an adaptive filter vibration active control method for simulating aircraft frame piezoelectric intelligent structure. The specific control system settings and operation methods are as follows:
[0081] (1) The piezoelectric sensor network ① and the piezoelectric drive network ② are arranged in the form of distributed patches on the surface of the aircraft frame structure, forming a multi-channel structural vibration control system with 8 inputs and 8 outputs;
[0082] (2) A set of excitation devices that generate external disturbances to the frame structure of the simulated aircraft. The general principle is: use a signal generator to generate ...
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