In this paper, a new method of control allocation is presented in the context of redundantly-actuated multirotor unmanned aerial vehicles (UAV). The equation between the virtual control efforts and the output of the actuator and the output limit of the actuator are taken as the constraints to express the method as a non-linear convex optimization problem. The proposed method is applied to extreme cases including poor actuator performance and propeller damage of multirotor and is suitable for redistributing the control effort to actuators while respecting its mechanical constraints.
Control Allocation for Multirotor Subjected to a Complete Actuator Failure
Lect. Notes Electrical Eng.
International Conference on Autonomous Unmanned Systems ; 2021 ; Changsha, China September 24, 2021 - September 26, 2021
Proceedings of 2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021) ; Kapitel : 222 ; 2249-2256
2022-03-18
8 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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