Thrust distribution method based on combination of particle swarm and sequential quadratic programming
A technology of sequence quadratic programming and thrust distribution, applied in two-dimensional position/course control, instrument, control/adjustment system, etc., can solve problems such as large initial value and no optimal solution for initial value, etc., to achieve convenient Adjustment, high precision of optimization, and high precision of algorithm optimization
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[0043] Embodiments of the present invention are described in further detail below in conjunction with the accompanying drawings:
[0044] A thrust allocation method based on the combination of particle swarm and sequential quadratic programming, such as figure 1 shown, including the following steps:
[0045] Step 1. The thrust distribution unit obtains the current three-axis command τ of the controller from the controller, specifically including longitudinal force X, lateral force Y and yaw moment N, that is, τ=(X, Y, N) T ;
[0046] Step 2. Establish a dynamic positioning system thrust distribution model, whose mathematical description is:
[0047] τ=(X,Y,N) T =B(α)T
[0048] Among them, T=(T 1 , T 2 …T n ) T , represents the thrust of n propellers;
[0049] α=(α 1 ,α 2 …α n ), represents the azimuth angles of n propellers;
[0050]
[0051] (l xi , l yi ) represents the position of the i-th propeller relative to the center of rotation of the ship;
[0052]...
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