Mechanical arm posture robustness control method based on interference estimator
A technology of disturbance estimation and robust control, applied in the direction of adaptive control, general control system, control/regulation system, etc., which can solve problems such as production safety accidents, control system difficulties, and external interference
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Embodiment 1
[0139] Under the action of the interference estimator under the action of three different forms of interference, the function test of the elevation angle ε tracking the sinusoidal signal.
[0140] In the implementation of the experiment, the attitude angle tracking experiment of the manipulator under three different interference forms was done, and the model test result diagram was given, and the control parameters Differential estimator experimental parameter α=50, interference estimator time constant T=1, tracking signal ε d =5sin(0.3πt)+13(deg). image 3 , 4 and 5 represent the results of the three-degree-of-freedom manipulator without UDE, respectively, when there is no artificial disturbance, artificial suspension of heavy objects, and artificial wind disturbance. The experiment proves that the helicopter cannot effectively track the sinusoidal signal without the action of UDE. , the error is large. Image 6 , 7 and 8 represent the results of the three-degree-of-free...
Embodiment 2
[0142] The interference estimator under the action of three different forms of interference, the effect test of pitch angle θ tracking sinusoidal signal.
[0143] The three disturbance forms in the experiment implementation are the same as those in Example 1, and the control parameters Differential estimator experimental parameter α=50, tracking signal θ d =5sin0.05πt(deg), the interference estimator time constant T=1. Figure 9 , 10 11 and 11 represent the results of the three-degree-of-freedom manipulator without UDE, respectively, when there is no artificial disturbance, artificial hanging heavy object disturbance, and artificial wind disturbance. Figure 12 , 13 and 14 respectively represent the three-degree-of-freedom helicopter tracking attitude angle results when the system has UDE effect when there is no artificial disturbance, artificial suspension heavy object disturbance, and artificial wind disturbance.
[0144] Figure 14 When man-made external wind interfer...
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