2021
DOI: 10.7546/crabs.2021.12.11
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Particle Swarm Optimization Based Optimal PID Controller for Quadcopters

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Cited by 4 publications
(3 citation statements)
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“…Three of the outputs are position variables x, y and z, other three of the outputs are orientation variables ϴ, φ and ψ. The mathematical model of the quadcopter is as follows (Sonugur et al 2021):…”
Section: Mathematical Model Of Quadcoptermentioning
confidence: 99%
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“…Three of the outputs are position variables x, y and z, other three of the outputs are orientation variables ϴ, φ and ψ. The mathematical model of the quadcopter is as follows (Sonugur et al 2021):…”
Section: Mathematical Model Of Quadcoptermentioning
confidence: 99%
“…It is reported that simulation results agreed with real quadcopter experimental values. PSOoptimized PID control of quadcopter is implemented and tested for various disturbances by (Sonugur et al 2021). The studies in the literature are mostly based on classical controller architecture where the error signal which is the difference between reference and measured output is fed into the controller.…”
Section: Introductionmentioning
confidence: 99%
“…However, there are considerations that the PID method cannot be applied effectively in quadrotors due to its non-linear structure. According to these considerations, the PID method cannot always efficiently control systems due to changing conditions [11][12][13]. At this point, optimization methods may need to be included in the process to use the PID controller in nonlinear applications such as quadrotor.…”
Section: Introductionmentioning
confidence: 99%