2016
DOI: 10.1016/j.isatra.2015.11.007
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Visual-based quadrotor control by means of fuzzy cognitive maps

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Cited by 35 publications
(17 citation statements)
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“…However, there are few studies in literature that show the effectiveness of using the FCM approach in the main controller design. In [19], the controllers designed based on the FCM approach are successfully used in a visual-based control application of a quadrotor. In [20], embedded dynamic fuzzy cognitive maps are used for control of an industrial mixer and satisfactory performance results are obtained compared with a fuzzy logic controller.…”
Section: Introductionmentioning
confidence: 99%
“…However, there are few studies in literature that show the effectiveness of using the FCM approach in the main controller design. In [19], the controllers designed based on the FCM approach are successfully used in a visual-based control application of a quadrotor. In [20], embedded dynamic fuzzy cognitive maps are used for control of an industrial mixer and satisfactory performance results are obtained compared with a fuzzy logic controller.…”
Section: Introductionmentioning
confidence: 99%
“…In control applications, the FCM approach is generally used for the support or design of supervisory controllers [18][19][20]. It is very rare to use the FCM approach to design a main controller for process control applications [21][22][23][24][25]. In [21], the FCM method is used as the main controller for the temperature and humidity control of a room in winter and summer operation season.…”
Section: Introductionmentioning
confidence: 99%
“…In [23], the main controller based on the FCM structure is designed for control of a heatex process. FCM based controllers are designed for the path tracking application of an unmanned air vehicle in [24]. In [25], three different FCM based controller models are proposed in the PI controller form, and their effective performances are shown by performing simulation studies on a nonlinear system.…”
Section: Introductionmentioning
confidence: 99%
“…All the multirotors are propelled by rotors and their amount are up to their configurations [19]. In terms of dynamics modeling, conventional works have derived multirotor dynamics using a linear thruster model as T = k t 2 ([1]- [10], [8], [14]- [18]), where T and Q represent thrust and reacting torque generated by a single propeller, respectively; Besides, k t and k q represent thrust and reacting torque coefficients; and is the rotation speed of the propeller. This thruster model contains two implications: (1) k t and k q are constant in all of the flight state; and (2) the propeller only generates force T and torque Q continuously without any generating other secondary forces and moments.…”
Section: Introductionmentioning
confidence: 99%