A control method based on UAV attitude control filter unit
A filter unit and control method technology, applied in the direction of attitude control, etc., can solve problems such as insufficient consideration of multi-source interference, achieve the effect of improving overall performance and overcoming multi-source interference
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[0029] like figure 1 Shown is the UAV attitude control filter unit and method principle diagram of the present invention, the filter unit of the present invention includes a UAV attitude control mathematical model, an anti-interference filter and an optimal controller; the anti-interference of the present invention The filtering method first establishes a mathematical model of UAV attitude considering various disturbance moments and noises, and uses its output as the input of the designed anti-jamming filter. The estimated value of the state variables in the mathematical model of UAV attitude and the mathematical model of external disturbance The estimated value of the model state variables is sent to the designed optimal controller, and the output of the optimal controller is turned on to the anti-jamming filter and the mathematical model of the UAV attitude control loop for feedback control.
[0030] like figure 2 As shown, the UAV attitude control anti-interference filter...
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