Novel unmanned aerial vehicle attitude system integral sliding mode control method based on disturbance observer
A technology of disturbance observer and integral sliding mode, which is applied in attitude control, control/adjustment system, non-electric variable control, etc., can solve the problems of large transient performance, reduce the weakening of transient performance, and solve the problem of UAV parameters Inaccurate, the effect of narrowing large errors
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[0053] In order to make the purpose, technical solution and advantages of the present application clearer, the present application will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present application, and are not intended to limit the present application.
[0054] In one embodiment, such as figure 1 As shown, a novel UAV attitude system integral sliding mode control method based on disturbance observer is provided, and the application of this method to UAV is taken as an example to illustrate, including the following steps:
[0055] Step S220, acquiring parameter errors and external disturbances observed by the disturbance observer in real time.
[0056] Among them, the disturbance observer is used to observe the parameter error and external disturbance of the drone, so that the control effect of the drone is better.
[005...
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