High-rise fire-fighting multi-unmanned aerial vehicle sliding-mode tracking control method and system under unknown disturbance
A tracking control, multi-UAV technology, applied in the control/regulation system, non-electric variable control, vehicle position/route/altitude control, etc., can solve the stability and performance degradation of UAV swarms and the hidden dangers of high-level fire rescue. , UAV communication discontinuity and other problems, to achieve the effect of achieving coordinated and stable flight, eliminating influence and reducing energy consumption
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Embodiment 1
[0061] In a typical embodiment of the present invention, such as figure 1 As shown, an adaptive sliding mode tracking control method for high-level firefighting multi-UAVs under unknown disturbance is proposed, which includes the following steps:
[0062] S1: Establish a mathematical model of the nominal system of high-rise fire-fighting UAVs under disturbance conditions;
[0063] S2: Determine the network communication topology between each UAV during the UAV swarm tracking control process;
[0064] S3: For the i-th following UAV nominal system, define the appropriate consistent position tracking error and consistent velocity tracking error;
[0065] S4: Based on the event trigger function and adaptive sliding mode control theory, a new type of sliding mode surface is designed. Based on this, an adaptive sliding mode tracking control law for a single fire-fighting UAV under unknown disturbance is constructed to eliminate the impact of external disturbance on no The impact o...
Embodiment 2
[0126] This embodiment provides a multi-UAV adaptive sliding mode tracking control system under unknown disturbance, including:
[0127] The first module is used to establish the mathematical model of the nominal system of the UAV under the disturbance situation;
[0128] The second module is used to determine the network communication topology between the UAVs during the UAV swarm tracking control process;
[0129] The third module is used to determine the collaborative consistency position tracking error and the collaborative consistency speed tracking error for the i-th following UAV nominal system according to the network communication topology;
[0130] The fourth module is used to determine the distributed integral sliding mode surface, and construct the adaptive sliding mode tracking control law of a single UAV under unknown disturbance, so as to control the position and speed of the following UAV to track the leading UAV.
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