2018 22nd International Conference on System Theory, Control and Computing (ICSTCC) 2018
DOI: 10.1109/icstcc.2018.8540660
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Experimental Validation of Quadrotors Angular Stability in a Gyroscopic Test Bench

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Cited by 14 publications
(8 citation statements)
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“…The EMMR platform can be used as a common four-rotor (quadrotor) experimental aircraft [ 23 , 25 ] for testing different control methods of underactuated systems [ 27 , 28 ]. Configurations with more than four rotors can also be assembled, such as hexarotor [ 29 ] used for teaching fault-tolerant control.…”
Section: Discussionmentioning
confidence: 99%
See 1 more Smart Citation
“…The EMMR platform can be used as a common four-rotor (quadrotor) experimental aircraft [ 23 , 25 ] for testing different control methods of underactuated systems [ 27 , 28 ]. Configurations with more than four rotors can also be assembled, such as hexarotor [ 29 ] used for teaching fault-tolerant control.…”
Section: Discussionmentioning
confidence: 99%
“…There are various papers that deal with the identification of propulsion parameters using test bench systems [ 20 , 21 ]. Furthermore, several approaches are investigated for the purpose of multirotor performance testing with experimental test rigs with three degrees of freedom (DOF) [ 22 , 23 ]. For the education purpose, experimental bench designs that can be made easily and cheaply are preferred, such as the setup presented in [ 24 ], and that can be easily upgraded with load cell sensors as presented in research [ 25 ].…”
Section: Introductionmentioning
confidence: 99%
“…The contributions of this paper are a consequence of previously published works by the authors, which have been studied for a long time. The main area of research concerns the aerial vehicle, coming from traditional multi-rotors to tilt-rotors, modeling, fault-tolerant control, controller design and tuning, and electromagnetic inference on the UAVs, among others [16,29,30,[39][40][41][42][43][44][45][46].…”
Section: Contributionsmentioning
confidence: 99%
“…UAV angular stability in three degrees of freedom, in terms of rolling, pitching, and yawing was the target measurement of the gyroscopic test bench developed in [94]. The platform consists of a gyroscopic support including a base where a ring-shaped structure is fastened and attached to a pivotal coupling, used as the UAV placement basis [94]. The test bench makes the UAV able to rotate in all directions.…”
Section: Ground Testmentioning
confidence: 99%
“…It is possible to place the center of gravity of the UAV at a lower height with respect to the gyroscopic base rotation axis of the system to be stable, as it functions as a simple pendulum, returning to its rest position or regulating the height to create both marginally stable (when the center of gravity position coincides with the rotation axis) and unstable (when the center of gravity is above the system rotation axis and operates as an inverted pendulum) conditions. In this way, it can be observed and manipulated the behavior of under or overactuated UAVs in adverse conditions [94].…”
Section: Ground Testmentioning
confidence: 99%