Method for controlling double UAVs (unmanned aerial vehicles) to cooperatively hoist rod-shaped rigid load
A technology of dual UAVs and control methods, applied in general control systems, adaptive control, control/regulation systems, etc., can solve the problems of inability to fully apply UAV systems, difficulties in experimental verification, and a large number of variables.  Good practical application significance, good load swing, and the effect of load swing suppression
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[0050] 1. Dynamic modeling of dual-UAV collaborative lifting system:
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[0056] Here, the selected system parameters are as follows:
[0057] m 1 = m 2 =3kg,m 3 =20kg,J 1 =J 2 =7kg·m 2 , l 1 = l 2 =2m, a=5m, g=9.8m / s 2
[0058] 2. Design of UAV outer loop controller
[0059] By deriving the outer loop Lyapunov function (21), the control input structure can be designed as follows:
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[0064] Among them, the expected positions of the two UAVs are set as [y d1 z d1 ] T =[7 10] T ,[y d2 z d2 ] T =[1210] T , and the expected angles of rope swing angle and load swing angle are θ 1d = θ 2d = θ 3d = 0°. k a1 ,k a2 ,k d1 ,k d2 ,k d3 ,k d4 is a positive control gain, using the control inputs (23) and (24) designed by the outer loop controller, it can realize the fixed-point hovering of the drone, eliminate the load swing and control the distance between t...
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