Fixed-wing unmanned aerial vehicle robust discrete fractional order control method considering external wind interference
A technology of fractional-order control and unmanned aerial vehicles, which is applied in the direction of attitude control, non-electric variable control, control/regulation system, etc. It can solve problems such as wind disturbance, system performance deterioration, and control law that is difficult to achieve performance indicators.
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[0076] Embodiments of the invention are described in detail below, examples of which are illustrated in the accompanying drawings. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.
[0077] Such as figure 1 As shown, the present invention provides a robust discrete fractional set control method that enables the fixed-wing UAV to not only maintain stability under the influence of external wind disturbance, but also track the desired reference trajectory. The control method is specifically divided into the following steps:
[0078] (1) According to the Newton-Euler theorem, establish the fixed-wing UAV longitudinal flight control system and attitude dynamics system model under the influence of external wind interference;
[0079] (2) Using the Euler approximation method to convert the continuous form UAV nonlinear model with wind interference into a ...
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