Hurwitz-stability-based sliding mode stabilization control method for underactuated unmanned surface vehicle
A stabilization control, unmanned boat technology, applied in the directions of adaptive control, general control system, control/regulation system, etc., can solve the underactuated characteristic, the control method is difficult to stabilize the control method of the unmanned boat, and does not meet the Brockett lemma conditions And other issues
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Embodiment 1
[0054] The purpose of the present invention is to overcome the environmental interference problem and the controller convergence performance optimization problem in the stabilization control of the unmanned boat, and provides a sliding mode stabilization control method for the underactuated unmanned boat based on Hurwitz stability. The control method fully considers the environmental disturbance factors in the stabilization control of the unmanned vehicle, and designs the sliding mode parameters according to the Hurwitz stability condition to obtain a robust sliding mode controller with exponential convergence characteristics.
[0055] In order to achieve the above object, the present invention adopts the following technical solutions:
[0056] The first step is to establish the stability control error equation of the unmanned vehicle, including the establishment of the kinematics and dynamics model of the control object and the environmental disturbance model:
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Embodiment 2
[0095] combined with figure 1 , a sliding mode stabilization control method for underactuated unmanned vehicles based on Hurwitz stability, the following steps are carried out:
[0096] Step 1, establishing the error equation of the unmanned vehicle stabilization control, including establishing the kinematics and dynamics model of the control object and the environmental disturbance model, and performing coordinate conversion to obtain the original stabilization control error equation:
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[0103] The above formula is the three-degree-of-freedom kinematics and dynamics equation of the unmanned vehicle horizontal plane, where m 11 ,m 22 ,m 33 , d 11 , d 22 , d 33 is the hydrodynamic coefficient, η=[x,y,ψ] T Indicates the position and heading angle of the UAV in the geodetic coordinate system, υ=[u,v,r] T is the longitudinal velocity, lateral velocity and heading angular velocity of the unmanned boat, τ=...
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