Landing Trajectory Design for UAV Considering Control Restrictions and Landing Speed
Keyword(s):
The article presents a method for designing the trajectory of the UAV in space, taking into account the restriction on control. The chosen optimal controls are namely normal overload with restrictions, tangential overload with restrictions, and lateral overload. The Pontryagin maximum principle allows the transition of the optimal control problem to a boundary value problem. The parameter continuation method is applied to solve the boundary problem. The article results reveal reference trajectories in different cases of UAV landing. This result allows the design of reference trajectories for the UAV to attain the highest landing efficiency.
2021 ◽
Vol 53
(3)
◽
pp. 380-394
2021 ◽
Vol 31
(2)
◽
pp. 265-284
2016 ◽
Vol 6
(1)
◽
pp. 53-61
◽
1992 ◽
Vol 45
(2)
◽
pp. 305-326
◽
2020 ◽
Vol 0
(0)
◽
Keyword(s):
2014 ◽
Vol 29
(1)
◽
pp. 67-85
◽
2019 ◽
Vol 25
(1)
◽
pp. 1
◽